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 45134U 26145.45932689 +.00000000 +00000-0 +15567-2 0 00000
2 45134 87.8854 40.8078 0001869 75.9546 284.1789 13.10375533 06
| Epoch (UTC): | 25 May 2026 11:01:25 |
| Eccentricity: | 0.0001869 |
| inclination: | 87.8854° |
| perigee height: | 1220 km |
| apogee height: | 1223 km |
| right ascension of ascending node: | 40.8078° |
| argument of perigee: | 75.9546° |
| revolutions per day: | 13.10375533 |
| mean anomaly at epoch: | 284.1789° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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