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 65320U 26145.64645205 +.00000000 +00000-0 +10835-3 0 00009
2 65320 97.7380 221.2659 0008291 246.0250 114.0101 14.92568063 00
| Epoch (UTC): | 25 May 2026 15:30:53 |
| Eccentricity: | 0.0008291 |
| inclination: | 97.7380° |
| perigee height: | 584 km |
| apogee height: | 596 km |
| right ascension of ascending node: | 221.2659° |
| argument of perigee: | 246.0250° |
| revolutions per day: | 14.92568063 |
| mean anomaly at epoch: | 114.0101° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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