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 65785U 26145.41154876 +.00000000 +00000-0 +31617-3 0 00009
2 65785 51.8984 41.2413 0000975 176.1300 183.9669 14.76656586 08
| Epoch (UTC): | 25 May 2026 09:52:37 |
| Eccentricity: | 0.0000975 |
| inclination: | 51.8984° |
| perigee height: | 639 km |
| apogee height: | 641 km |
| right ascension of ascending node: | 41.2413° |
| argument of perigee: | 176.1300° |
| revolutions per day: | 14.76656586 |
| mean anomaly at epoch: | 183.9669° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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