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 45254U 26144.04062306 +.00000000 +00000-0 +00000-0 0 00001
2 45254 65.5249 321.5337 6864967 278.3237 15.0398 2.00601922 03
| Epoch (UTC): | 24 May 2026 00:58:29 |
| Eccentricity: | 0.6864967 |
| inclination: | 65.5249° |
| perigee height: | 1948 km |
| apogee height: | 38410 km |
| right ascension of ascending node: | 321.5337° |
| argument of perigee: | 278.3237° |
| revolutions per day: | 2.00601922 |
| mean anomaly at epoch: | 15.0398° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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