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 45162U 26145.45282589 +.00000000 +00000-0 +81553-3 0 00007
2 45162 87.8856 40.8042 0001897 73.6200 286.5135 13.10371864 07
| Epoch (UTC): | 25 May 2026 10:52:04 |
| Eccentricity: | 0.0001897 |
| inclination: | 87.8856° |
| perigee height: | 1220 km |
| apogee height: | 1223 km |
| right ascension of ascending node: | 40.8042° |
| argument of perigee: | 73.6200° |
| revolutions per day: | 13.10371864 |
| mean anomaly at epoch: | 286.5135° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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