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 60293U 26145.03677905 +.00000000 +00000-0 +33845-4 0 00005
2 60293 53.1607 57.5072 0001248 82.0990 278.0152 15.30193239 04
| Epoch (UTC): | 25 May 2026 00:52:57 |
| Eccentricity: | 0.0001248 |
| inclination: | 53.1607° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 57.5072° |
| argument of perigee: | 82.0990° |
| revolutions per day: | 15.30193239 |
| mean anomaly at epoch: | 278.0152° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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