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 45144U 26145.13223117 +.00000000 +00000-0 -11947-2 0 00004
2 45144 87.8873 40.8646 0002050 81.2334 278.9025 13.09823949 08
| Epoch (UTC): | 25 May 2026 03:10:24 |
| Eccentricity: | 0.0002050 |
| inclination: | 87.8873° |
| perigee height: | 1222 km |
| apogee height: | 1225 km |
| right ascension of ascending node: | 40.8646° |
| argument of perigee: | 81.2334° |
| revolutions per day: | 13.09823949 |
| mean anomaly at epoch: | 278.9025° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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