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 67286U 26145.61983316 +.00000000 +00000-0 +35112-3 0 00002
2 67286 97.3941 220.8612 0011212 78.6903 281.5594 15.23830541 01
| Epoch (UTC): | 25 May 2026 14:52:33 |
| Eccentricity: | 0.0011212 |
| inclination: | 97.3941° |
| perigee height: | 487 km |
| apogee height: | 502 km |
| right ascension of ascending node: | 220.8612° |
| argument of perigee: | 78.6903° |
| revolutions per day: | 15.23830541 |
| mean anomaly at epoch: | 281.5594° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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