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 07647U 26087.75790402 +.00000000 +00000-0 +58094-4 0 00004
2 07647 49.8246 265.3660 0217173 341.1714 18.1239 13.82335885 09
| Epoch (UTC): | 28 March 2026 18:11:22 |
| Eccentricity: | 0.0217173 |
| inclination: | 49.8246° |
| perigee height: | 796 km |
| apogee height: | 1115 km |
| right ascension of ascending node: | 265.3660° |
| argument of perigee: | 341.1714° |
| revolutions per day: | 13.82335885 |
| mean anomaly at epoch: | 18.1239° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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