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 53031U 26145.26106437 +.00000000 +00000-0 +20081-4 0 00007
2 53031 53.2125 90.3783 0001180 81.7115 278.4011 15.08841210 08
| Epoch (UTC): | 25 May 2026 06:15:55 |
| Eccentricity: | 0.0001180 |
| inclination: | 53.2125° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 90.3783° |
| argument of perigee: | 81.7115° |
| revolutions per day: | 15.08841210 |
| mean anomaly at epoch: | 278.4011° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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