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 65247U 26145.57998752 +.00000000 +00000-0 +22493-3 0 00000
2 65247 97.4475 188.3086 0001873 117.0297 243.1122 15.05656945 03
| Epoch (UTC): | 25 May 2026 13:55:10 |
| Eccentricity: | 0.0001873 |
| inclination: | 97.4475° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 188.3086° |
| argument of perigee: | 117.0297° |
| revolutions per day: | 15.05656945 |
| mean anomaly at epoch: | 243.1122° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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