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 53244U 26145.60607337 +.00000000 +00000-0 +36548-4 0 00001
2 53244 53.2120 218.9072 0001301 79.1561 280.9577 15.08842186 07
| Epoch (UTC): | 25 May 2026 14:32:44 |
| Eccentricity: | 0.0001301 |
| inclination: | 53.2120° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 218.9072° |
| argument of perigee: | 79.1561° |
| revolutions per day: | 15.08842186 |
| mean anomaly at epoch: | 280.9577° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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