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 67894U 26145.54535382 +.00000000 +00000-0 +74390-3 0 00006
2 67894 97.2846 79.0246 0001994 91.4740 268.6731 15.33487291 04
| Epoch (UTC): | 25 May 2026 13:05:18 |
| Eccentricity: | 0.0001994 |
| inclination: | 97.2846° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 79.0246° |
| argument of perigee: | 91.4740° |
| revolutions per day: | 15.33487291 |
| mean anomaly at epoch: | 268.6731° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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