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 67864U 26145.43494628 +.00000000 +00000-0 +63499-3 0 00006
2 67864 53.1595 207.9176 0001379 54.8247 305.2883 15.30218254 03
| Epoch (UTC): | 25 May 2026 10:26:19 |
| Eccentricity: | 0.0001379 |
| inclination: | 53.1595° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 207.9176° |
| argument of perigee: | 54.8247° |
| revolutions per day: | 15.30218254 |
| mean anomaly at epoch: | 305.2883° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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