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 45454U 26145.62900720 +.00000000 +00000-0 -84621-3 0 00004
2 45454 87.8917 25.5531 0001793 80.4614 279.6716 13.10935887 01
| Epoch (UTC): | 25 May 2026 15:05:46 |
| Eccentricity: | 0.0001793 |
| inclination: | 87.8917° |
| perigee height: | 1218 km |
| apogee height: | 1221 km |
| right ascension of ascending node: | 25.5531° |
| argument of perigee: | 80.4614° |
| revolutions per day: | 13.10935887 |
| mean anomaly at epoch: | 279.6716° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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