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 26104.20934146 +.00000000 +00000-0 +16659-3 0 00002
2 00115 48.1627 55.5405 0026754 329.3654 30.5701 14.97847387 01
| Epoch (UTC): | 14 April 2026 05:01:27 |
| Eccentricity: | 0.0026754 |
| inclination: | 48.1627° |
| perigee height: | 555 km |
| apogee height: | 592 km |
| right ascension of ascending node: | 55.5405° |
| argument of perigee: | 329.3654° |
| revolutions per day: | 14.97847387 |
| mean anomaly at epoch: | 30.5701° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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