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 67249U 26145.43074728 +.00000000 +00000-0 +24238-3 0 00006
2 67249 97.5123 212.4514 0294196 49.5267 313.1191 14.74131881 07
| Epoch (UTC): | 25 May 2026 10:20:16 |
| Eccentricity: | 0.0294196 |
| inclination: | 97.5123° |
| perigee height: | 441 km |
| apogee height: | 855 km |
| right ascension of ascending node: | 212.4514° |
| argument of perigee: | 49.5267° |
| revolutions per day: | 14.74131881 |
| mean anomaly at epoch: | 313.1191° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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