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 60093U 26145.11473541 +.00000000 +00000-0 -46958-5 0 00003
2 60093 53.1608 42.4116 0001231 81.3478 278.7662 15.30196812 03
| Epoch (UTC): | 25 May 2026 02:45:13 |
| Eccentricity: | 0.0001231 |
| inclination: | 53.1608° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 42.4116° |
| argument of perigee: | 81.3478° |
| revolutions per day: | 15.30196812 |
| mean anomaly at epoch: | 278.7662° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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