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 26134.14446706 +.00000000 +00000-0 +14065-3 0 00003
2 26069 70.9978 22.7871 0012031 331.8368 28.2101 14.13893367 00
| Epoch (UTC): | 14 May 2026 03:28:01 |
| Eccentricity: | 0.0012031 |
| inclination: | 70.9978° |
| perigee height: | 837 km |
| apogee height: | 855 km |
| right ascension of ascending node: | 22.7871° |
| argument of perigee: | 331.8368° |
| revolutions per day: | 14.13893367 |
| mean anomaly at epoch: | 28.2101° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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