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 67902U 26145.37407399 +.00000000 +00000-0 +76100-3 0 00004
2 67902 97.2834 78.9518 0002347 108.5728 251.5770 15.33451187 09
| Epoch (UTC): | 25 May 2026 08:58:39 |
| Eccentricity: | 0.0002347 |
| inclination: | 97.2834° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 78.9518° |
| argument of perigee: | 108.5728° |
| revolutions per day: | 15.33451187 |
| mean anomaly at epoch: | 251.5770° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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