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 26041.88856568 +.00000000 +00000-0 +46567-4 0 00005
2 26069 70.9920 216.2155 0009702 128.8531 231.3459 14.13866053 04
| Epoch (UTC): | 10 February 2026 21:19:32 |
| Eccentricity: | 0.0009702 |
| inclination: | 70.9920° |
| perigee height: | 839 km |
| apogee height: | 853 km |
| right ascension of ascending node: | 216.2155° |
| argument of perigee: | 128.8531° |
| revolutions per day: | 14.13866053 |
| mean anomaly at epoch: | 231.3459° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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