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 67255U 26145.20517257 +.00000000 +00000-0 +19043-3 0 00005
2 67255 97.2868 214.3398 0069979 54.1489 306.6212 15.06994695 02
| Epoch (UTC): | 25 May 2026 04:55:26 |
| Eccentricity: | 0.0069979 |
| inclination: | 97.2868° |
| perigee height: | 497 km |
| apogee height: | 594 km |
| right ascension of ascending node: | 214.3398° |
| argument of perigee: | 54.1489° |
| revolutions per day: | 15.06994695 |
| mean anomaly at epoch: | 306.6212° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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