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 67880U 26145.55352729 +.00000000 +00000-0 +62977-3 0 00002
2 67880 97.2846 79.0115 0002081 93.0178 267.1303 15.33443418 07
| Epoch (UTC): | 25 May 2026 13:17:04 |
| Eccentricity: | 0.0002081 |
| inclination: | 97.2846° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 79.0115° |
| argument of perigee: | 93.0178° |
| revolutions per day: | 15.33443418 |
| mean anomaly at epoch: | 267.1303° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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