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 26073.60006060 +.00000000 +00000-0 +83997-4 0 00004
2 44881 97.7603 148.1218 0014615 42.8077 317.4274 14.86351712 05
| Epoch (UTC): | 14 March 2026 14:24:05 |
| Eccentricity: | 0.0014615 |
| inclination: | 97.7603° |
| perigee height: | 599 km |
| apogee height: | 620 km |
| right ascension of ascending node: | 148.1218° |
| argument of perigee: | 42.8077° |
| revolutions per day: | 14.86351712 |
| mean anomaly at epoch: | 317.4274° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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