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 00115U 26130.49073375 +.00000000 +00000-0 +20586-3 0 00004
2 00115 48.1632 286.2952 0025493 88.7985 271.5854 14.97994253 00
| Epoch (UTC): | 10 May 2026 11:46:39 |
| Eccentricity: | 0.0025493 |
| inclination: | 48.1632° |
| perigee height: | 555 km |
| apogee height: | 591 km |
| right ascension of ascending node: | 286.2952° |
| argument of perigee: | 88.7985° |
| revolutions per day: | 14.97994253 |
| mean anomaly at epoch: | 271.5854° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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