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 65261U 26145.61425251 +.00000000 +00000-0 +22859-3 0 00006
2 65261 97.5211 272.9743 0014906 45.2932 314.9512 15.15224244 01
| Epoch (UTC): | 25 May 2026 14:44:31 |
| Eccentricity: | 0.0014906 |
| inclination: | 97.5211° |
| perigee height: | 510 km |
| apogee height: | 531 km |
| right ascension of ascending node: | 272.9743° |
| argument of perigee: | 45.2932° |
| revolutions per day: | 15.15224244 |
| mean anomaly at epoch: | 314.9512° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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