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 67899U 26145.36591793 +.00000000 +00000-0 +56827-3 0 00004
2 67899 97.2842 78.9595 0002351 103.3635 256.7870 15.33448623 02
| Epoch (UTC): | 25 May 2026 08:46:55 |
| Eccentricity: | 0.0002351 |
| inclination: | 97.2842° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 78.9595° |
| argument of perigee: | 103.3635° |
| revolutions per day: | 15.33448623 |
| mean anomaly at epoch: | 256.7870° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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