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 26069U 26071.67377995 +.00000000 +00000-0 +77698-4 0 00006
2 26069 70.9969 153.7697 0008913 70.8467 289.3619 14.13883819 00
| Epoch (UTC): | 12 March 2026 16:10:14 |
| Eccentricity: | 0.0008913 |
| inclination: | 70.9969° |
| perigee height: | 840 km |
| apogee height: | 853 km |
| right ascension of ascending node: | 153.7697° |
| argument of perigee: | 70.8467° |
| revolutions per day: | 14.13883819 |
| mean anomaly at epoch: | 289.3619° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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