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 37153U 26161.61720654 +.00000000 +00000-0 +63375-3 0 00006
2 37153 82.4573 82.5116 0008685 94.3155 265.8916 12.40792204 05
| Epoch (UTC): | 10 June 2026 14:48:46 |
| Eccentricity: | 0.0008685 |
| inclination: | 82.4573° |
| perigee height: | 1496 km |
| apogee height: | 1510 km |
| right ascension of ascending node: | 82.5116° |
| argument of perigee: | 94.3155° |
| revolutions per day: | 12.40792204 |
| mean anomaly at epoch: | 265.8916° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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