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 67027U 26145.34389990 +.00000000 +00000-0 +30901-3 0 00004
2 67027 70.0008 261.0291 0003163 267.4749 92.6048 14.98349388 08
| Epoch (UTC): | 25 May 2026 08:15:12 |
| Eccentricity: | 0.0003163 |
| inclination: | 70.0008° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 261.0291° |
| argument of perigee: | 267.4749° |
| revolutions per day: | 14.98349388 |
| mean anomaly at epoch: | 92.6048° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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