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 67733U 26145.60246660 +.00000000 +00000-0 +78757-3 0 00004
2 67733 97.2841 199.1238 0001027 92.3399 267.7962 15.33453597 01
| Epoch (UTC): | 25 May 2026 14:27:33 |
| Eccentricity: | 0.0001027 |
| inclination: | 97.2841° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 199.1238° |
| argument of perigee: | 92.3399° |
| revolutions per day: | 15.33453597 |
| mean anomaly at epoch: | 267.7962° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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