View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 57621U 26145.03100262 +.00000000 +00000-0 -47355-5 0 00006
2 57621 43.0047 10.2897 0001285 271.4023 88.6681 15.27588494 03
| Epoch (UTC): | 25 May 2026 00:44:38 |
| Eccentricity: | 0.0001285 |
| inclination: | 43.0047° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 10.2897° |
| argument of perigee: | 271.4023° |
| revolutions per day: | 15.27588494 |
| mean anomaly at epoch: | 88.6681° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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