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 65608U 26145.59283865 +.00000000 +00000-0 +22714-2 0 00000
2 65608 97.4465 214.0990 0002242 123.4401 236.7041 15.05711556 01
| Epoch (UTC): | 25 May 2026 14:13:41 |
| Eccentricity: | 0.0002242 |
| inclination: | 97.4465° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 214.0990° |
| argument of perigee: | 123.4401° |
| revolutions per day: | 15.05711556 |
| mean anomaly at epoch: | 236.7041° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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