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 61665U 26145.24926862 +.00000000 +00000-0 +14224-4 0 00001
2 61665 53.1613 95.7194 0001278 89.0621 271.0527 15.30189833 09
| Epoch (UTC): | 25 May 2026 05:58:56 |
| Eccentricity: | 0.0001278 |
| inclination: | 53.1613° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 95.7194° |
| argument of perigee: | 89.0621° |
| revolutions per day: | 15.30189833 |
| mean anomaly at epoch: | 271.0527° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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