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 44968U 26145.63823951 +.00000000 +00000-0 +95273-3 0 00008
2 44968 53.1506 304.9322 0001514 292.4713 67.6135 15.48559217 00
| Epoch (UTC): | 25 May 2026 15:19:03 |
| Eccentricity: | 0.0001514 |
| inclination: | 53.1506° |
| perigee height: | 420 km |
| apogee height: | 422 km |
| right ascension of ascending node: | 304.9322° |
| argument of perigee: | 292.4713° |
| revolutions per day: | 15.48559217 |
| mean anomaly at epoch: | 67.6135° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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