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 53980U 26145.51081337 +.00000000 +00000-0 +10863-5 0 00007
2 53980 53.2144 233.9789 0000884 24.8545 335.2490 15.08836699 06
| Epoch (UTC): | 25 May 2026 12:15:34 |
| Eccentricity: | 0.0000884 |
| inclination: | 53.2144° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 233.9789° |
| argument of perigee: | 24.8545° |
| revolutions per day: | 15.08836699 |
| mean anomaly at epoch: | 335.2490° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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