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 68672U 26145.39801601 +.00000000 +00000-0 +30891-3 0 00002
2 68672 97.2861 16.9660 0001415 93.4532 266.6873 15.33453252 00
| Epoch (UTC): | 25 May 2026 09:33:08 |
| Eccentricity: | 0.0001415 |
| inclination: | 97.2861° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 16.9660° |
| argument of perigee: | 93.4532° |
| revolutions per day: | 15.33453252 |
| mean anomaly at epoch: | 266.6873° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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