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 61133U 26099.89311610 +.00000000 +00000-0 +71480-3 0 00005
2 61133 88.9442 274.7569 0079808 118.2936 242.6357 14.56096262 03
| Epoch (UTC): | 09 April 2026 21:26:05 |
| Eccentricity: | 0.0079808 |
| inclination: | 88.9442° |
| perigee height: | 649 km |
| apogee height: | 762 km |
| right ascension of ascending node: | 274.7569° |
| argument of perigee: | 118.2936° |
| revolutions per day: | 14.56096262 |
| mean anomaly at epoch: | 242.6357° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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