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 67248U 26145.62023772 +.00000000 +00000-0 +12183-3 0 00005
2 67248 97.5435 211.7403 0278816 49.5530 312.9632 14.67217903 04
| Epoch (UTC): | 25 May 2026 14:53:08 |
| Eccentricity: | 0.0278816 |
| inclination: | 97.5435° |
| perigee height: | 473 km |
| apogee height: | 866 km |
| right ascension of ascending node: | 211.7403° |
| argument of perigee: | 49.5530° |
| revolutions per day: | 14.67217903 |
| mean anomaly at epoch: | 312.9632° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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