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 61712U 26145.62002338 +.00000000 +00000-0 +23008-4 0 00009
2 61712 53.1604 104.1001 0001375 84.4168 275.6989 15.30192238 02
| Epoch (UTC): | 25 May 2026 14:52:50 |
| Eccentricity: | 0.0001375 |
| inclination: | 53.1604° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 104.1001° |
| argument of perigee: | 84.4168° |
| revolutions per day: | 15.30192238 |
| mean anomaly at epoch: | 275.6989° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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