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 60294U 26145.53895583 +.00000000 +00000-0 +14522-2 0 00004
2 60294 53.1614 55.6672 0001793 53.8037 306.3129 15.30550390 05
| Epoch (UTC): | 25 May 2026 12:56:05 |
| Eccentricity: | 0.0001793 |
| inclination: | 53.1614° |
| perigee height: | 473 km |
| apogee height: | 475 km |
| right ascension of ascending node: | 55.6672° |
| argument of perigee: | 53.8037° |
| revolutions per day: | 15.30550390 |
| mean anomaly at epoch: | 306.3129° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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