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 60259U 26145.48774299 +.00000000 +00000-0 +94923-4 0 00004
2 60259 53.1614 55.9440 0001373 80.8474 279.2682 15.30206815 03
| Epoch (UTC): | 25 May 2026 11:42:20 |
| Eccentricity: | 0.0001373 |
| inclination: | 53.1614° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 55.9440° |
| argument of perigee: | 80.8474° |
| revolutions per day: | 15.30206815 |
| mean anomaly at epoch: | 279.2682° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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