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 67572U 26145.61940456 +.00000000 +00000-0 +38511-3 0 00004
2 67572 97.2856 205.9409 0000241 95.7461 264.3809 15.33450854 04
| Epoch (UTC): | 25 May 2026 14:51:56 |
| Eccentricity: | 0.0000241 |
| inclination: | 97.2856° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 205.9409° |
| argument of perigee: | 95.7461° |
| revolutions per day: | 15.33450854 |
| mean anomaly at epoch: | 264.3809° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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