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 67873U 26145.45093341 +.00000000 +00000-0 +63905-3 0 00007
2 67873 53.1585 205.8867 0001252 85.5896 274.5250 15.34387587 03
| Epoch (UTC): | 25 May 2026 10:49:20 |
| Eccentricity: | 0.0001252 |
| inclination: | 53.1585° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 205.8867° |
| argument of perigee: | 85.5896° |
| revolutions per day: | 15.34387587 |
| mean anomaly at epoch: | 274.5250° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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