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 67901U 26145.38494788 +.00000000 +00000-0 +37580-3 0 00001
2 67901 97.2850 78.9340 0001392 95.4927 264.6474 15.33447103 02
| Epoch (UTC): | 25 May 2026 09:14:19 |
| Eccentricity: | 0.0001392 |
| inclination: | 97.2850° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 78.9340° |
| argument of perigee: | 95.4927° |
| revolutions per day: | 15.33447103 |
| mean anomaly at epoch: | 264.6474° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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