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 53897U 26145.66668980 +.00000000 +00000-0 +10270-1 0 00003
2 53897 53.2168 330.9906 0001011 76.2530 280.9768 15.49635959 01
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001011 |
| inclination: | 53.2168° |
| perigee height: | 417 km |
| apogee height: | 418 km |
| right ascension of ascending node: | 330.9906° |
| argument of perigee: | 76.2530° |
| revolutions per day: | 15.49635959 |
| mean anomaly at epoch: | 280.9768° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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