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 59107U 26145.62715477 +.00000000 +00000-0 +10648-3 0 00004
2 59107 97.8462 276.5793 0010175 77.2222 283.0136 14.96528382 06
| Epoch (UTC): | 25 May 2026 15:03:06 |
| Eccentricity: | 0.0010175 |
| inclination: | 97.8462° |
| perigee height: | 571 km |
| apogee height: | 585 km |
| right ascension of ascending node: | 276.5793° |
| argument of perigee: | 77.2222° |
| revolutions per day: | 14.96528382 |
| mean anomaly at epoch: | 283.0136° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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