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AISTECHSAT-2

In orbit NORAD 43768 MSIH-7029-5546-1995-2723 Spain

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

18

Observations all time

Mission information
Spacecraft name
AISTECHSAT-2
Frequency usage status
Violator
Status
Active
The satellite is in orbit
The network has not received data from this satellite for a long time
Launch and timeline
Carrier rocket
Falcon 9 Block 5
Spaceport
Space Launch Complex 4E
Launch time
2018-12-03 00:00:00
Separation time
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
511.63 km
Apogee
515.79 km
Inclination
97.4°
Period
95.0 min
Semi-major axis
6891.8 km
Velocity
7.59 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-11 12:56:42 UTC
Two-line elements (TLE)
1 43768U 18099L   26284.12917374  .00005773  00000-0  30042-3 0  9995
2 43768 97.4165 329.6231 0003049 246.4929 113.5984 15.16412686429848
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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 07:59:44 AISTECHSAT 2
NORAD 43768
OBJECT F
NORAD 61899
4.504 3.01 2.1e-07
2026-10-12 10:22:16 AISTECHSAT 2
NORAD 43768
OBJECT F
NORAD 61899
3.575 3.01 3.4e-07
2026-10-12 20:31:32 AISTECHSAT 2
NORAD 43768
COSMOS 2251 DEB
NORAD 38220
3.803 15.06 1.1e-07
2026-10-12 22:26:06 AISTECHSAT 2
NORAD 43768
STARLINK-6061
NORAD 56795
3.402 14.98 4.3e-06
2026-10-12 23:01:29 AISTECHSAT 2
NORAD 43768
ION SCV-020
NORAD 64545
2.039 8.43 9.0e-07
2026-10-14 20:57:47 AISTECHSAT 2
NORAD 43768
PVCC
NORAD 58025
4.065 4.00 2.6e-07
2026-10-15 08:04:57 AISTECHSAT 2
NORAD 43768
LEMUR-2-NEUROSPICY
NORAD 63355
2.294 8.67 7.1e-07
2026-10-15 21:54:31 AISTECHSAT 2
NORAD 43768
FENGYUN 1C DEB
NORAD 30520
4.354 15.05 8.3e-08
2026-10-16 02:44:57 AISTECHSAT 2
NORAD 43768
YAOGAN-37
NORAD 55244
4.423 14.18 1.1e-07
2026-10-17 16:57:50 AISTECHSAT 2
NORAD 43768
COSMOS 970 DEB
NORAD 20032
2.786 11.19 4.1e-07
2026-10-17 19:26:03 AISTECHSAT 2
NORAD 43768
COSMOS 1275 DEB
NORAD 42180
1.696 14.12 7.4e-07
2026-10-18 01:44:39 AISTECHSAT 2
NORAD 43768
PEGASUS DEB
NORAD 24091
2.604 10.70 4.9e-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