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GLOBAL-18

In orbit NORAD 52196 XKOT-2810-1157-1690-8027 United States of America

2022

Launch

2

Observations all time

Mission information
Spacecraft name
GLOBAL-18
Other names
2022-034B
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
2022-04-02 00:00:00
Separation time
2022-04-02 00:00:00
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
413.55 km
Apogee
417.31 km
Inclination
53.0°
Period
92.9 min
Semi-major axis
6793.4 km
Velocity
7.66 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-11 12:56:43 UTC
Two-line elements (TLE)
1 52196U 22034B   26284.11537898  .00041483  00000-0  71685-3 0  9998
2 52196 52.9808 60.8165 0002799 281.9398 78.1296 15.50584322254920
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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
2026-10-11 21:35:09 GLOBAL-18
NORAD 52196
SL-3 DEB
NORAD 14209
2.745 14.11 2.9e-07
2026-10-11 22:38:35 GLOBAL-18
NORAD 52196
STARLINK-38415
NORAD 100634
4.553 11.77 4.4e-06
2026-10-12 15:39:46 GLOBAL-18
NORAD 52196
STARLINK-38412
NORAD 100640
4.595 11.85 4.3e-06
2026-10-12 18:45:26 GLOBAL-18
NORAD 52196
STARLINK-38422
NORAD 100637
4.488 11.87 4.5e-06
2026-10-12 19:31:49 GLOBAL-18
NORAD 52196
STARLINK-38412
NORAD 100640
4.412 11.88 4.7e-06
2026-10-12 21:04:39 GLOBAL-18
NORAD 52196
STARLINK-38422
NORAD 100637
4.098 11.89 5.4e-06
2026-10-13 09:01:42 GLOBAL-18
NORAD 52196
COSMOS 1470
NORAD 14147
3.652 13.97 1.7e-07
2026-10-13 12:53:53 GLOBAL-18
NORAD 52196
COSMOS 1470
NORAD 14147
1.399 13.95 1.2e-06
2026-10-13 14:52:16 GLOBAL-18
NORAD 52196
STARLINK-38421
NORAD 100631
2.277 11.96 1.7e-05
2026-10-13 17:11:29 GLOBAL-18
NORAD 52196
STARLINK-38421
NORAD 100631
2.729 11.98 1.2e-05
2026-10-14 16:52:09 GLOBAL-18
NORAD 52196
STARLINK-31096
NORAD 58592
4.833 4.84 5.5e-06
2026-10-16 10:56:43 GLOBAL-18
NORAD 52196
STARLINK-38413
NORAD 100635
4.115 12.26 5.2e-06
2026-10-16 17:00:05 GLOBAL-18
NORAD 52196
CREW DRAGON 13
NORAD 100882
2.932 2.61 5.1e-07
2026-10-16 17:00:05 ISS (ZARYA)
NORAD 25544
GLOBAL-18
NORAD 52196
4.697 2.61 1.2e-05
2026-10-16 17:00:05 ISS (UNITY)
NORAD 25575
GLOBAL-18
NORAD 52196
4.697 2.61 2.5e-06
2026-10-16 17:00:05 ISS (ZVEZDA)
NORAD 26400
GLOBAL-18
NORAD 52196
4.697 2.61 1.5e-05
2026-10-16 17:00:05 ISS (DESTINY)
NORAD 26700
GLOBAL-18
NORAD 52196
4.697 2.61 1.9e-06
2026-10-16 17:00:05 POISK
NORAD 36086
GLOBAL-18
NORAD 52196
4.697 2.61 2.0e-07
2026-10-16 17:00:05 ISS (NAUKA)
NORAD 49044
GLOBAL-18
NORAD 52196
4.697 2.61 2.0e-07
2026-10-16 17:00:05 GLOBAL-18
NORAD 52196
PROGRESS-MS 34
NORAD 68837
4.697 2.61 2.0e-07
2026-10-16 17:00:05 GLOBAL-18
NORAD 52196
SOYUZ-MS 29
NORAD 100057
4.697 2.61 2.0e-07
2026-10-16 17:00:05 GLOBAL-18
NORAD 52196
PROGRESS-MS 35
NORAD 100712
4.697 2.61 2.0e-07
2026-10-17 00:52:08 GLOBAL-18
NORAD 52196
STARLINK-38436
NORAD 100641
4.473 12.32 4.4e-06

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