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 65757U 26145.50377369 +.00000000 +00000-0 +39779-3 0 00009
2 65757 53.1594 336.1301 0001438 90.1205 269.9961 15.30207395 06
| Epoch (UTC): | 25 May 2026 12:05:26 |
| Eccentricity: | 0.0001438 |
| inclination: | 53.1594° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 336.1301° |
| argument of perigee: | 90.1205° |
| revolutions per day: | 15.30207395 |
| mean anomaly at epoch: | 269.9961° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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