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 53680U 26145.37900972 +.00000000 +00000-0 +45690-3 0 00007
2 53680 97.4474 26.4231 0001875 74.2964 285.8470 15.05617170 07
| Epoch (UTC): | 25 May 2026 09:05:46 |
| Eccentricity: | 0.0001875 |
| inclination: | 97.4474° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 26.4231° |
| argument of perigee: | 74.2964° |
| revolutions per day: | 15.05617170 |
| mean anomaly at epoch: | 285.8470° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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