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

SENTINEL-1

In orbit NORAD 69897 TEAW-1621-8543-0676-6317 Germany

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

14

Observations all time

Mission information
Spacecraft name
SENTINEL-1
Other names
OSIRIS-A
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
2026-07-07 07:12:00
Separation time
2026-07-07 08:06:31
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
590.70 km
Apogee
593.41 km
Inclination
97.7°
Period
96.6 min
Semi-major axis
6970.2 km
Velocity
7.56 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 04:46:21 UTC
Two-line elements (TLE)
1 69897U 26156AE  26282.77788640  .00001197  00000-0  12685-3 0  9999
2 69897 97.7468 181.5351 0001949 155.0069 205.1244 14.90929214 14076
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
2026-10-11 19:16:41 SHIJIAN-16 (SJ-16)
NORAD 39358
SPEAR-1C
NORAD 69897
4.770 6.69 1.8e-07
2026-10-12 00:15:27 SPEAR-1C
NORAD 69897
ARIANE 5 R/B
NORAD 28499
2.361 9.82 6.3e-07
2026-10-12 17:08:13 IRIDE-MS2-HEO-13
NORAD 68985
SPEAR-1C
NORAD 69897
0.866 0.46 5.9e-06
2026-10-12 22:20:08 SPEAR-1C
NORAD 69897
CZ-6A DEB
NORAD 54632
4.023 14.97 9.8e-08
2026-10-13 00:50:38 BEIJING-3B
NORAD 53587
SPEAR-1C
NORAD 69897
2.691 14.98 2.2e-07
2026-10-13 01:52:01 SPEAR-1C
NORAD 69897
CZ-4B DEB
NORAD 39052
3.746 14.49 1.4e-07
2026-10-13 06:07:50 IRIDE-MS2-HEO-6
NORAD 64576
SPEAR-1C
NORAD 69897
4.099 14.31 1.2e-07
2026-10-13 06:56:08 IRIDE-MS2-HEO-6
NORAD 64576
SPEAR-1C
NORAD 69897
2.888 14.34 2.4e-07
2026-10-13 19:44:27 SPEAR-1C
NORAD 69897
DELTA 1 DEB
NORAD 9003
4.916 8.48 1.5e-07
2026-10-14 08:33:38 LEMUR-2-MARIO-SOUSA
NORAD 67365
SPEAR-1C
NORAD 69897
4.073 11.33 1.9e-07
2026-10-15 07:56:11 VINDLER 2.3
NORAD 68486
SPEAR-1C
NORAD 69897
4.844 7.23 1.7e-07
2026-10-16 16:08:56 SPEAR-1C
NORAD 69897
THOR BURNER 2A DEB
NORAD 37584
2.988 3.67 4.8e-07
2026-10-17 01:32:03 LEAP-1
NORAD 65321
SPEAR-1C
NORAD 69897
1.203 14.95 1.1e-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