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 26071.64777480 +.00000000 +00000-0 +16290-3 0 00008
2 44881 97.7604 146.2157 0014801 48.8484 311.4006 14.86351196 05
| Epoch (UTC): | 12 March 2026 15:32:47 |
| Eccentricity: | 0.0014801 |
| inclination: | 97.7604° |
| perigee height: | 599 km |
| apogee height: | 620 km |
| right ascension of ascending node: | 146.2157° |
| argument of perigee: | 48.8484° |
| revolutions per day: | 14.86351196 |
| mean anomaly at epoch: | 311.4006° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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