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 65684U 26145.57070017 +.00000000 +00000-0 +81204-3 0 00005
2 65684 53.1603 348.6232 0001339 88.5186 271.5968 15.30208492 01
| Epoch (UTC): | 25 May 2026 13:41:48 |
| Eccentricity: | 0.0001339 |
| inclination: | 53.1603° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 348.6232° |
| argument of perigee: | 88.5186° |
| revolutions per day: | 15.30208492 |
| mean anomaly at epoch: | 271.5968° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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