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 44800U 26145.59074846 +.00000000 +00000-0 +00000-0 0 00000
2 44800 0.0529 348.4809 0002038 90.9809 51.8816 1.00273613 00
| Epoch (UTC): | 25 May 2026 14:10:40 |
| Eccentricity: | 0.0002038 |
| inclination: | 0.0529° |
| perigee height: | 35777 km |
| apogee height: | 35795 km |
| right ascension of ascending node: | 348.4809° |
| argument of perigee: | 90.9809° |
| revolutions per day: | 1.00273613 |
| mean anomaly at epoch: | 51.8816° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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