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 26106.54408045 +.00000000 +00000-0 +16644-3 0 00009
2 00115 48.1636 44.0595 0026659 339.7223 20.2635 14.97855786 09
| Epoch (UTC): | 16 April 2026 13:03:28 |
| Eccentricity: | 0.0026659 |
| inclination: | 48.1636° |
| perigee height: | 555 km |
| apogee height: | 592 km |
| right ascension of ascending node: | 44.0595° |
| argument of perigee: | 339.7223° |
| revolutions per day: | 14.97855786 |
| mean anomaly at epoch: | 20.2635° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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