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 53716U 26145.36590896 +.00000000 +00000-0 -19613-4 0 00004
2 53716 53.2140 269.5827 0001440 90.3475 269.7682 15.08837924 02
| Epoch (UTC): | 25 May 2026 08:46:54 |
| Eccentricity: | 0.0001440 |
| inclination: | 53.2140° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 269.5827° |
| argument of perigee: | 90.3475° |
| revolutions per day: | 15.08837924 |
| mean anomaly at epoch: | 269.7682° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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