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 67724U 26145.56167170 +.00000000 +00000-0 +81679-3 0 00004
2 67724 97.2845 199.0297 0001563 320.0270 40.0857 15.33428349 05
| Epoch (UTC): | 25 May 2026 13:28:48 |
| Eccentricity: | 0.0001563 |
| inclination: | 97.2845° |
| perigee height: | 465 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 199.0297° |
| argument of perigee: | 320.0270° |
| revolutions per day: | 15.33428349 |
| mean anomaly at epoch: | 40.0857° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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