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 65248U 26145.35292552 +.00000000 +00000-0 +35258-3 0 00005
2 65248 97.4463 188.1556 0001558 122.5443 237.5935 15.05658518 02
| Epoch (UTC): | 25 May 2026 08:28:12 |
| Eccentricity: | 0.0001558 |
| inclination: | 97.4463° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 188.1556° |
| argument of perigee: | 122.5443° |
| revolutions per day: | 15.05658518 |
| mean anomaly at epoch: | 237.5935° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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