Satellite Tracking, Prediction and Informations about

Objects in the Sky

Search Tips
You can search by Satellite Name, Norad ID or any other keyword that it is included in satellite description.

You can search for object debris if you search by word DEB and for Rocket Bodies if you search by the keyword R/B country.

Good Luck

Track Random satellites:
ESSA 2 (OT-2)
SL-8 R/B

Track INTERCOSMOS 24 Satellite in Real Time

Detailed information about INTERCOSMOS 24 satellite

Designator id: 1989-080A

Description of INTERCOSMOS 24 Satellite:

The Active mission, consisting of the Soviet Active spacecraft and the closely orbiting Czech subsatellite Magion 2, had the main objectives of better understanding of the radiation properties of loop antennas in a plasma environment, spatial structure of E-M fields in the near zone, non-linear effects in the near zone, propagation and non-linear effects of whistler modes, triggered particle precipitation and triggered waves, and detection of ground-based VLF transmissions. Active was triaxially stabilized, with a 14 meter boom providing stability of the vertical axis, and the other axes stabilized by gas jets. The stabilization ensured that the plane of the loop antenna, fed by a 10 kW, 10 kHz transmitter, remained in the orbital plane. Attitude profile was telemetered along with other data. An onboard tape recorder could carry 60 Mb of data. It carried two separate batteries, charged by solar panels: one for the high power VLF transmitter and the other for all other instruments. The VLF battery was charged for several hours, before each session of many minutes long transmission. The other active experiment was the many releases of Xenon gas to test the so called Critical Velocity Ionization. The relative distance between Active and Magion 2 could be maneuvered and determined with a precision of 100 meters by means of lidar tracking. The main objectives of the mission remained unrealized because of the mis-deployed VLF loop antenna; the radiated power was estimated to be no more than about 50 W. The operation schedules of the Active mission were coordinated with the many NASA (and other)-sponsored investigations of the magnetosphere.

Technical data:

Launch Date: 1989-09-28
Launch Vehicle: Cyclone
Launch Site: Tyuratam (Baikonur Cosmodrome), U.S.S.R
Mass: 1570.0 kg

Funding Agencies:

Institut Kosmicheskich Issledovaniy(Inst. of Cosmophysical Research) (U.S.S.R)


Space Physics

Source: Nasa

Two Line Element Set (TLE):
1 20261U 89080A   12339.15386707  .00000530  00000-0  15992-3 0  9235
2 20261 082.5931 001.7781 1211011 311.4192 038.8782 12.54214895 58205

Last TLE update on :2012-12-04

Find more details about INTERCOSMOS 24 Satellite