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 65514U 26145.36040648 +.00000000 +00000-0 +64876-3 0 00007
2 65514 53.1605 275.2196 0001553 134.9588 225.1539 15.30206803 02
| Epoch (UTC): | 25 May 2026 08:38:59 |
| Eccentricity: | 0.0001553 |
| inclination: | 53.1605° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 275.2196° |
| argument of perigee: | 134.9588° |
| revolutions per day: | 15.30206803 |
| mean anomaly at epoch: | 225.1539° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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