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 65239U 26145.38338043 +.00000000 +00000-0 +34671-3 0 00002
2 65239 97.4497 188.1134 0001839 131.9795 228.1590 15.05657811 05
| Epoch (UTC): | 25 May 2026 09:12:04 |
| Eccentricity: | 0.0001839 |
| inclination: | 97.4497° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 188.1134° |
| argument of perigee: | 131.9795° |
| revolutions per day: | 15.05657811 |
| mean anomaly at epoch: | 228.1590° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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