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 65507U 26145.34879998 +.00000000 +00000-0 +57836-3 0 00003
2 65507 53.1601 275.1579 0001307 79.4115 280.7033 15.30213328 06
| Epoch (UTC): | 25 May 2026 08:22:16 |
| Eccentricity: | 0.0001307 |
| inclination: | 53.1601° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 275.1579° |
| argument of perigee: | 79.4115° |
| revolutions per day: | 15.30213328 |
| mean anomaly at epoch: | 280.7033° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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