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 53290U 26145.55996044 +.00000000 +00000-0 +98366-4 0 00008
2 53290 53.2159 199.0394 0001041 76.1424 283.9684 15.08883056 05
| Epoch (UTC): | 25 May 2026 13:26:20 |
| Eccentricity: | 0.0001041 |
| inclination: | 53.2159° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 199.0394° |
| argument of perigee: | 76.1424° |
| revolutions per day: | 15.08883056 |
| mean anomaly at epoch: | 283.9684° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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