RU | EN | ZH --:-- UTC Sign in

YOUTHSAT

In orbit NORAD 37388 WQYT-3877-9353-7434-8931 India

2011

Launch

32

Observations all time

Mission information
Spacecraft name
YOUTHSAT
Status
Active
The satellite is in orbit
The network has not received data from this satellite for a long time
Launch and timeline
Launch time
2011-04-20 00:00:00
Separation time
Last observers
Observer
Time of receipt
2024-12-08 13:46:17 UTC
2024-12-08 12:08:58 UTC
2024-12-08 10:30:13 UTC
2024-12-08 08:53:04 UTC
2024-12-08 07:16:48 UTC
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
792.82 km
Apogee
813.94 km
Inclination
98.4°
Period
101.0 min
Semi-major axis
7181.5 km
Velocity
7.43 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-11 12:56:42 UTC
Two-line elements (TLE)
1 37388U 11015B   26284.15993515  .00000177  00000-0  92227-4 0  9998
2 37388 98.3852 253.0726 0014682 6.3485 4.2192 14.25669721804168
Copy content
Orbit history, past year

Mean elements of every TLE set over the past 365 days, plotted against the epoch of the set. Each source is its own line; click it in the legend to hide it. A jump in altitude is a manoeuvre or a bad set; lines drifting apart are a disagreement between sources. “TLE age” is how many hours have passed since the epoch of the source's freshest set, plotted against when the set reached us, on a logarithmic scale. A set the source repeats unchanged does not reset the age.

Prediction divergence

Each TLE set is propagated with SGP4 to the epoch of the next set from the same source and compared with it, plotted against the epoch of the next set; the tooltip shows how many hours ahead the prediction ran. The logarithmic scale shows the size of the divergence and the tooltip its sign: plus along-track means the prediction is ahead of the satellite. This is how well the sets agree, not the true error: the reference is a TLE too, off by about a kilometre. An outlier is a manoeuvre between sets. Sets more than a week apart are not compared.

Time of closest approach, UTC Object 1 Object 2 Distance, km Speed, km/s Max. probability
2026-10-12 06:27:23 YOUTHSAT
NORAD 37388
CZ-4C R/B
NORAD 39242
3.851 9.51 2.4e-07
2026-10-12 07:59:14 YOUTHSAT
NORAD 37388
QUAKESAT
NORAD 27845
2.256 4.84 8.3e-07
2026-10-12 09:30:29 YOUTHSAT
NORAD 37388
FENGYUN 1C DEB
NORAD 30145
4.476 14.43 8.9e-08
2026-10-12 16:26:28 YOUTHSAT
NORAD 37388
DMSP 5D-2 F13 DEB
NORAD 40478
2.099 2.03 9.9e-07
2026-10-13 12:34:52 YOUTHSAT
NORAD 37388
CZ-4C DEB
NORAD 43411
4.695 12.09 1.3e-07
2026-10-14 01:12:50 YOUTHSAT
NORAD 37388
FENGYUN 1C DEB
NORAD 30173
4.935 11.86 1.2e-07
2026-10-14 06:09:13 YOUTHSAT
NORAD 37388
FENGYUN 1C DEB
NORAD 37714
2.561 14.42 2.7e-07
2026-10-14 07:09:10 YOUTHSAT
NORAD 37388
METEOR 2-5 DEB
NORAD 45511
2.814 14.78 2.0e-07
2026-10-14 15:49:38 YOUTHSAT
NORAD 37388
CZ-6A DEB
NORAD 60816
4.616 1.55 2.1e-07
2026-10-14 20:11:10 YOUTHSAT
NORAD 37388
COSMOS 2251 DEB
NORAD 35583
4.112 14.97 8.9e-08
2026-10-14 22:06:28 YOUTHSAT
NORAD 37388
THOR ABLESTAR DEB
NORAD 19302
0.269 5.59 5.7e-05
2026-10-14 22:18:06 YOUTHSAT
NORAD 37388
CZ-6A DEB
NORAD 54305
4.253 7.05 2.2e-07
2026-10-15 03:22:50 YOUTHSAT
NORAD 37388
COSMOS 1275 DEB
NORAD 15768
3.114 14.36 1.9e-07
2026-10-15 08:24:53 YOUTHSAT
NORAD 37388
CZ-6A DEB
NORAD 54407
3.969 4.82 2.7e-07
2026-10-15 10:06:14 YOUTHSAT
NORAD 37388
FENGYUN 1C DEB
NORAD 30068
4.921 2.18 1.8e-07
2026-10-15 17:39:25 YOUTHSAT
NORAD 37388
IRS-P2
NORAD 23323
4.955 9.79 1.1e-06
2026-10-16 21:34:07 YOUTHSAT
NORAD 37388
SL-16 DEB
NORAD 22351
4.109 12.95 1.5e-07
2026-10-17 00:56:07 YOUTHSAT
NORAD 37388
SL-3 R/B
NORAD 11289
2.948 14.90 4.6e-07
2026-10-17 16:45:03 YOUTHSAT
NORAD 37388
FENGYUN 1C DEB
NORAD 29754
1.003 13.87 2.1e-06
2026-10-17 22:08:11 YOUTHSAT
NORAD 37388
METEOR 2-5 DEB
NORAD 45510
3.062 14.88 1.6e-07
2026-10-18 03:44:32 YOUTHSAT
NORAD 37388
COSMOS 2251 DEB
NORAD 47052
2.789 13.33 3.0e-07

Data: CelesTrak SOCRATES Plus, computed from TLEs of the public catalog. This is an estimate, not grounds for a manoeuvre: TLEs carry no covariance, and the maximum probability assumes a position error.

All conjunctions of this satellite