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 45141U 26145.39970881 +.00000000 +00000-0 +13998-2 0 00003
2 45141 87.8851 40.8068 0002342 78.8766 281.2624 13.10371627 09
| Epoch (UTC): | 25 May 2026 09:35:34 |
| Eccentricity: | 0.0002342 |
| inclination: | 87.8851° |
| perigee height: | 1220 km |
| apogee height: | 1224 km |
| right ascension of ascending node: | 40.8068° |
| argument of perigee: | 78.8766° |
| revolutions per day: | 13.10371627 |
| mean anomaly at epoch: | 281.2624° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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