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 45151U 26145.42721661 +.00000000 +00000-0 +15740-2 0 00005
2 45151 87.8919 25.5861 0001870 78.7101 281.4237 13.11415743 04
| Epoch (UTC): | 25 May 2026 10:15:11 |
| Eccentricity: | 0.0001870 |
| inclination: | 87.8919° |
| perigee height: | 1216 km |
| apogee height: | 1219 km |
| right ascension of ascending node: | 25.5861° |
| argument of perigee: | 78.7101° |
| revolutions per day: | 13.11415743 |
| mean anomaly at epoch: | 281.4237° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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