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 67717U 26145.55299623 +.00000000 +00000-0 +55632-3 0 00004
2 67717 97.2845 257.1889 0000919 93.4706 266.6642 15.33451780 02
| Epoch (UTC): | 25 May 2026 13:16:18 |
| Eccentricity: | 0.0000919 |
| inclination: | 97.2845° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 257.1889° |
| argument of perigee: | 93.4706° |
| revolutions per day: | 15.33451780 |
| mean anomaly at epoch: | 266.6642° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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