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 44057U 26145.53008185 +.00000000 +00000-0 +16216-3 0 00000
2 44057 87.9106 233.2835 0002299 92.4563 267.6832 13.16593850 05
| Epoch (UTC): | 25 May 2026 12:43:19 |
| Eccentricity: | 0.0002299 |
| inclination: | 87.9106° |
| perigee height: | 1196 km |
| apogee height: | 1200 km |
| right ascension of ascending node: | 233.2835° |
| argument of perigee: | 92.4563° |
| revolutions per day: | 13.16593850 |
| mean anomaly at epoch: | 267.6832° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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