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 57653U 26145.33236656 +.00000000 +00000-0 +13222-3 0 00004
2 57653 43.0059 9.0074 0001086 263.9051 96.1677 15.27570221 08
| Epoch (UTC): | 25 May 2026 07:58:36 |
| Eccentricity: | 0.0001086 |
| inclination: | 43.0059° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 9.0074° |
| argument of perigee: | 263.9051° |
| revolutions per day: | 15.27570221 |
| mean anomaly at epoch: | 96.1677° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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