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 44344U 26061.03416727 +.00000000 +00000-0 +00000-0 0 00007
2 44344 42.3156 29.8401 1969602 329.8441 20.1319 4.54376646 01
| Epoch (UTC): | 02 March 2026 00:49:12 |
| Eccentricity: | 0.1969602 |
| inclination: | 42.3156° |
| perigee height: | 5987 km |
| apogee height: | 12052 km |
| right ascension of ascending node: | 29.8401° |
| argument of perigee: | 329.8441° |
| revolutions per day: | 4.54376646 |
| mean anomaly at epoch: | 20.1319° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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