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 53016U 26145.13870677 +.00000000 +00000-0 -14085-4 0 00008
2 53016 53.2131 100.9277 0001218 91.1154 268.9978 15.08844826 06
| Epoch (UTC): | 25 May 2026 03:19:44 |
| Eccentricity: | 0.0001218 |
| inclination: | 53.2131° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 100.9277° |
| argument of perigee: | 91.1154° |
| revolutions per day: | 15.08844826 |
| mean anomaly at epoch: | 268.9978° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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