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 45451U 26145.37111434 +.00000000 +00000-0 -51781-3 0 00000
2 45451 87.8925 25.5785 0001970 74.1156 286.0189 13.11414260 00
| Epoch (UTC): | 25 May 2026 08:54:24 |
| Eccentricity: | 0.0001970 |
| inclination: | 87.8925° |
| perigee height: | 1216 km |
| apogee height: | 1219 km |
| right ascension of ascending node: | 25.5785° |
| argument of perigee: | 74.1156° |
| revolutions per day: | 13.11414260 |
| mean anomaly at epoch: | 286.0189° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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