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 55815U 26145.39439214 +.00000000 +00000-0 +68261-3 0 00006
2 55815 87.8942 294.2544 0001885 95.4988 264.6357 13.14502099 06
| Epoch (UTC): | 25 May 2026 09:27:55 |
| Eccentricity: | 0.0001885 |
| inclination: | 87.8942° |
| perigee height: | 1204 km |
| apogee height: | 1207 km |
| right ascension of ascending node: | 294.2544° |
| argument of perigee: | 95.4988° |
| revolutions per day: | 13.14502099 |
| mean anomaly at epoch: | 264.6357° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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