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 67281U 26145.45872317 +.00000000 +00000-0 +20980-3 0 00004
2 67281 97.3885 220.3658 0013601 82.7264 277.5518 15.22278084 06
| Epoch (UTC): | 25 May 2026 11:00:33 |
| Eccentricity: | 0.0013601 |
| inclination: | 97.3885° |
| perigee height: | 490 km |
| apogee height: | 508 km |
| right ascension of ascending node: | 220.3658° |
| argument of perigee: | 82.7264° |
| revolutions per day: | 15.22278084 |
| mean anomaly at epoch: | 277.5518° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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