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 44881U 26072.65757815 +.00000000 +00000-0 +98430-4 0 00007
2 44881 97.7604 147.2017 0014696 45.7451 314.4969 14.86351122 03
| Epoch (UTC): | 13 March 2026 15:46:54 |
| Eccentricity: | 0.0014696 |
| inclination: | 97.7604° |
| perigee height: | 599 km |
| apogee height: | 620 km |
| right ascension of ascending node: | 147.2017° |
| argument of perigee: | 45.7451° |
| revolutions per day: | 14.86351122 |
| mean anomaly at epoch: | 314.4969° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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