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 67895U 26145.53449223 +.00000000 +00000-0 +32746-3 0 00003
2 67895 97.2853 79.0390 0001590 87.1853 272.9572 15.33444617 08
| Epoch (UTC): | 25 May 2026 12:49:40 |
| Eccentricity: | 0.0001590 |
| inclination: | 97.2853° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 79.0390° |
| argument of perigee: | 87.1853° |
| revolutions per day: | 15.33444617 |
| mean anomaly at epoch: | 272.9572° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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