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 67208U 26145.54495963 +.00000000 +00000-0 +25255-3 0 00001
2 67208 70.0018 340.8092 0002429 267.8302 92.2579 14.98334942 03
| Epoch (UTC): | 25 May 2026 13:04:44 |
| Eccentricity: | 0.0002429 |
| inclination: | 70.0018° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 340.8092° |
| argument of perigee: | 267.8302° |
| revolutions per day: | 14.98334942 |
| mean anomaly at epoch: | 92.2579° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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