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 26669U 26087.38964793 +.00000000 +00000-0 +44171-2 0 00003
2 26669 100.1202 129.0398 0030310 40.5525 336.0030 13.88230185 01
| Epoch (UTC): | 28 March 2026 09:21:05 |
| Eccentricity: | 0.0030310 |
| inclination: | 100.1202° |
| perigee height: | 913 km |
| apogee height: | 957 km |
| right ascension of ascending node: | 129.0398° |
| argument of perigee: | 40.5525° |
| revolutions per day: | 13.88230185 |
| mean anomaly at epoch: | 336.0030° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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