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 68391U 26145.36565220 +.00000000 +00000-0 +48482-3 0 00006
2 68391 97.2848 287.8929 0001243 82.2393 277.8991 15.33456122 04
| Epoch (UTC): | 25 May 2026 08:46:32 |
| Eccentricity: | 0.0001243 |
| inclination: | 97.2848° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 287.8929° |
| argument of perigee: | 82.2393° |
| revolutions per day: | 15.33456122 |
| mean anomaly at epoch: | 277.8991° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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