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 53008U 26145.29602367 +.00000000 +00000-0 +23220-4 0 00005
2 53008 53.2136 110.2130 0001317 75.0339 285.0798 15.08843956 03
| Epoch (UTC): | 25 May 2026 07:06:16 |
| Eccentricity: | 0.0001317 |
| inclination: | 53.2136° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 110.2130° |
| argument of perigee: | 75.0339° |
| revolutions per day: | 15.08843956 |
| mean anomaly at epoch: | 285.0798° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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