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 62848U 26145.34169560 +.00000000 +00000-0 +68496-3 0 00009
2 62848 43.0020 16.1111 0001043 281.1854 78.8880 15.27598752 07
| Epoch (UTC): | 25 May 2026 08:12:02 |
| Eccentricity: | 0.0001043 |
| inclination: | 43.0020° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 16.1111° |
| argument of perigee: | 281.1854° |
| revolutions per day: | 15.27598752 |
| mean anomaly at epoch: | 78.8880° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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