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 62093U 26145.43787308 +.00000000 +00000-0 +25683-2 0 00007
2 62093 42.9993 300.4639 0002395 265.8050 94.2544 15.71009582 04
| Epoch (UTC): | 25 May 2026 10:30:32 |
| Eccentricity: | 0.0002395 |
| inclination: | 42.9993° |
| perigee height: | 354 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 300.4639° |
| argument of perigee: | 265.8050° |
| revolutions per day: | 15.71009582 |
| mean anomaly at epoch: | 94.2544° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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