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 65712U 26145.43476308 +.00000000 +00000-0 +22344-3 0 00005
2 65712 49.9883 41.0009 0013101 160.2725 199.8726 14.92711720 03
| Epoch (UTC): | 25 May 2026 10:26:03 |
| Eccentricity: | 0.0013101 |
| inclination: | 49.9883° |
| perigee height: | 580 km |
| apogee height: | 599 km |
| right ascension of ascending node: | 41.0009° |
| argument of perigee: | 160.2725° |
| revolutions per day: | 14.92711720 |
| mean anomaly at epoch: | 199.8726° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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