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 67010U 26145.33955419 +.00000000 +00000-0 +32436-3 0 00005
2 67010 70.0008 261.0143 0003437 268.4859 91.5906 14.98340726 01
| Epoch (UTC): | 25 May 2026 08:08:57 |
| Eccentricity: | 0.0003437 |
| inclination: | 70.0008° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 261.0143° |
| argument of perigee: | 268.4859° |
| revolutions per day: | 14.98340726 |
| mean anomaly at epoch: | 91.5906° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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