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 67794U 26145.57118909 +.00000000 +00000-0 +33485-3 0 00000
2 67794 51.8841 213.7515 0018068 316.9310 43.0257 15.23878109 07
| Epoch (UTC): | 25 May 2026 13:42:30 |
| Eccentricity: | 0.0018068 |
| inclination: | 51.8841° |
| perigee height: | 482 km |
| apogee height: | 507 km |
| right ascension of ascending node: | 213.7515° |
| argument of perigee: | 316.9310° |
| revolutions per day: | 15.23878109 |
| mean anomaly at epoch: | 43.0257° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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