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 26134.35931762 +.00000000 +00000-0 +20481-3 0 00000
2 00115 48.1626 267.2671 0025438 106.7253 253.6460 14.98012476 01
| Epoch (UTC): | 14 May 2026 08:37:25 |
| Eccentricity: | 0.0025438 |
| inclination: | 48.1626° |
| perigee height: | 555 km |
| apogee height: | 591 km |
| right ascension of ascending node: | 267.2671° |
| argument of perigee: | 106.7253° |
| revolutions per day: | 14.98012476 |
| mean anomaly at epoch: | 253.6460° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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