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 68665U 26145.61009755 +.00000000 +00000-0 +50963-3 0 00001
2 68665 97.2860 17.1380 0002130 92.0039 268.1448 15.33456188 01
| Epoch (UTC): | 25 May 2026 14:38:32 |
| Eccentricity: | 0.0002130 |
| inclination: | 97.2860° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 17.1380° |
| argument of perigee: | 92.0039° |
| revolutions per day: | 15.33456188 |
| mean anomaly at epoch: | 268.1448° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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