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 26158.70344726 +.00000000 +00000-0 +30347-3 0 00005
2 00115 48.1610 147.5162 0026278 217.2506 142.6590 14.98154421 09
| Epoch (UTC): | 07 June 2026 16:52:57 |
| Eccentricity: | 0.0026278 |
| inclination: | 48.1610° |
| perigee height: | 554 km |
| apogee height: | 591 km |
| right ascension of ascending node: | 147.5162° |
| argument of perigee: | 217.2506° |
| revolutions per day: | 14.98154421 |
| mean anomaly at epoch: | 142.6590° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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