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 53007U 26145.22610644 +.00000000 +00000-0 +24460-4 0 00001
2 53007 53.2143 110.5364 0001426 101.8966 258.2186 15.08844578 01
| Epoch (UTC): | 25 May 2026 05:25:35 |
| Eccentricity: | 0.0001426 |
| inclination: | 53.2143° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 110.5364° |
| argument of perigee: | 101.8966° |
| revolutions per day: | 15.08844578 |
| mean anomaly at epoch: | 258.2186° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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