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 55246U 26145.00981677 +.00000000 +00000-0 +00000-0 0 00001
2 55246 5.3268 64.3557 0011362 305.9783 217.8992 0.99057257 08
| Epoch (UTC): | 25 May 2026 00:14:08 |
| Eccentricity: | 0.0011362 |
| inclination: | 5.3268° |
| perigee height: | 36082 km |
| apogee height: | 36179 km |
| right ascension of ascending node: | 64.3557° |
| argument of perigee: | 305.9783° |
| revolutions per day: | 0.99057257 |
| mean anomaly at epoch: | 217.8992° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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