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 60358U 26145.50220348 +.00000000 +00000-0 +14888-3 0 00009
2 60358 53.1606 313.1282 0001104 96.2807 263.8320 15.30209487 06
| Epoch (UTC): | 25 May 2026 12:03:10 |
| Eccentricity: | 0.0001104 |
| inclination: | 53.1606° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 313.1282° |
| argument of perigee: | 96.2807° |
| revolutions per day: | 15.30209487 |
| mean anomaly at epoch: | 263.8320° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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