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 65544U 26145.49217987 +.00000000 +00000-0 +11243-3 0 00006
2 65544 85.9902 51.5727 0014902 135.6680 224.5708 14.26473286 02
| Epoch (UTC): | 25 May 2026 11:48:44 |
| Eccentricity: | 0.0014902 |
| inclination: | 85.9902° |
| perigee height: | 793 km |
| apogee height: | 814 km |
| right ascension of ascending node: | 51.5727° |
| argument of perigee: | 135.6680° |
| revolutions per day: | 14.26473286 |
| mean anomaly at epoch: | 224.5708° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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