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 65319U 26145.60715247 +.00000000 +00000-0 +12092-3 0 00004
2 65319 97.7325 221.1228 0007917 172.6039 187.5298 14.92870421 07
| Epoch (UTC): | 25 May 2026 14:34:17 |
| Eccentricity: | 0.0007917 |
| inclination: | 97.7325° |
| perigee height: | 583 km |
| apogee height: | 595 km |
| right ascension of ascending node: | 221.1228° |
| argument of perigee: | 172.6039° |
| revolutions per day: | 14.92870421 |
| mean anomaly at epoch: | 187.5298° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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