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 45152U 26145.24175683 +.00000000 +00000-0 +17327-2 0 00006
2 45152 87.8858 40.8327 0001886 75.6096 284.5240 13.10412402 06
| Epoch (UTC): | 25 May 2026 05:48:07 |
| Eccentricity: | 0.0001886 |
| inclination: | 87.8858° |
| perigee height: | 1220 km |
| apogee height: | 1223 km |
| right ascension of ascending node: | 40.8327° |
| argument of perigee: | 75.6096° |
| revolutions per day: | 13.10412402 |
| mean anomaly at epoch: | 284.5240° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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