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 65576U 26143.02718094 +.00000000 +00000-0 -14623-3 0 00009
2 65576 81.3009 34.1803 0004751 263.8752 96.1863 13.82825318 05
| Epoch (UTC): | 23 May 2026 00:39:08 |
| Eccentricity: | 0.0004751 |
| inclination: | 81.3009° |
| perigee height: | 950 km |
| apogee height: | 957 km |
| right ascension of ascending node: | 34.1803° |
| argument of perigee: | 263.8752° |
| revolutions per day: | 13.82825318 |
| mean anomaly at epoch: | 96.1863° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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