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 45449U 26145.39994285 +.00000000 +00000-0 -65682-3 0 00007
2 45449 87.8913 25.5884 0001648 80.8792 279.2523 13.11417232 04
| Epoch (UTC): | 25 May 2026 09:35:55 |
| Eccentricity: | 0.0001648 |
| inclination: | 87.8913° |
| perigee height: | 1216 km |
| apogee height: | 1219 km |
| right ascension of ascending node: | 25.5884° |
| argument of perigee: | 80.8792° |
| revolutions per day: | 13.11417232 |
| mean anomaly at epoch: | 279.2523° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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