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 67813U 26145.49100174 +.00000000 +00000-0 +69690-3 0 00005
2 67813 97.2856 333.6256 0001747 104.4876 255.6561 15.33454920 07
| Epoch (UTC): | 25 May 2026 11:47:02 |
| Eccentricity: | 0.0001747 |
| inclination: | 97.2856° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 333.6256° |
| argument of perigee: | 104.4876° |
| revolutions per day: | 15.33454920 |
| mean anomaly at epoch: | 255.6561° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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