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 44868U 26145.54280769 +.00000000 +00000-0 +00000-0 0 00002
2 44868 0.0129 297.0259 0000183 191.2834 100.2337 1.00269117 01
| Epoch (UTC): | 25 May 2026 13:01:38 |
| Eccentricity: | 0.0000183 |
| inclination: | 0.0129° |
| perigee height: | 35787 km |
| apogee height: | 35788 km |
| right ascension of ascending node: | 297.0259° |
| argument of perigee: | 191.2834° |
| revolutions per day: | 1.00269117 |
| mean anomaly at epoch: | 100.2337° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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