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 60921U 26145.41672976 +.00000000 +00000-0 +42502-4 0 00008
2 60921 53.1616 287.3485 0001103 94.0788 266.0339 15.30197721 05
| Epoch (UTC): | 25 May 2026 10:00:05 |
| Eccentricity: | 0.0001103 |
| inclination: | 53.1616° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 287.3485° |
| argument of perigee: | 94.0788° |
| revolutions per day: | 15.30197721 |
| mean anomaly at epoch: | 266.0339° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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