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 44076U 26145.52770512 +.00000000 +00000-0 +00000-0 0 00001
2 44076 0.4834 83.0775 0000913 319.9405 107.0927 1.00271489 04
| Epoch (UTC): | 25 May 2026 12:39:53 |
| Eccentricity: | 0.0000913 |
| inclination: | 0.4834° |
| perigee height: | 35783 km |
| apogee height: | 35791 km |
| right ascension of ascending node: | 83.0775° |
| argument of perigee: | 319.9405° |
| revolutions per day: | 1.00271489 |
| mean anomaly at epoch: | 107.0927° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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