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 65573U 26143.61778623 +.00000000 +00000-0 -39073-4 0 00002
2 65573 81.3017 33.5115 0005556 263.8511 96.2012 13.83916437 08
| Epoch (UTC): | 23 May 2026 14:49:36 |
| Eccentricity: | 0.0005556 |
| inclination: | 81.3017° |
| perigee height: | 946 km |
| apogee height: | 954 km |
| right ascension of ascending node: | 33.5115° |
| argument of perigee: | 263.8511° |
| revolutions per day: | 13.83916437 |
| mean anomaly at epoch: | 96.2012° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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