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 67100U 26145.37202626 +.00000000 +00000-0 +32094-3 0 00004
2 67100 70.0011 181.1052 0003553 266.5871 93.4882 14.98347570 06
| Epoch (UTC): | 25 May 2026 08:55:43 |
| Eccentricity: | 0.0003553 |
| inclination: | 70.0011° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 181.1052° |
| argument of perigee: | 266.5871° |
| revolutions per day: | 14.98347570 |
| mean anomaly at epoch: | 93.4882° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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