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 65813U 26145.37646924 +.00000000 +00000-0 +24219-3 0 00006
2 65813 97.4527 8.2335 0001881 75.1119 285.0316 15.05658234 06
| Epoch (UTC): | 25 May 2026 09:02:06 |
| Eccentricity: | 0.0001881 |
| inclination: | 97.4527° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 8.2335° |
| argument of perigee: | 75.1119° |
| revolutions per day: | 15.05658234 |
| mean anomaly at epoch: | 285.0316° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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