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 65854U 26145.58335647 +.00000000 +00000-0 -44647-3 0 00009
2 65854 53.1587 296.6637 0000956 95.3059 256.1109 15.34393560 02
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0000956 |
| inclination: | 53.1587° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 296.6637° |
| argument of perigee: | 95.3059° |
| revolutions per day: | 15.34393560 |
| mean anomaly at epoch: | 256.1109° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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