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 39215U 26144.94699058 +.00000000 +00000-0 +00000-0 0 00000
2 39215 2.9966 1.5512 0002004 45.7805 200.9411 1.00276140 01
| Epoch (UTC): | 24 May 2026 22:43:39 |
| Eccentricity: | 0.0002004 |
| inclination: | 2.9966° |
| perigee height: | 35777 km |
| apogee height: | 35794 km |
| right ascension of ascending node: | 1.5512° |
| argument of perigee: | 45.7805° |
| revolutions per day: | 1.00276140 |
| mean anomaly at epoch: | 200.9411° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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