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 27640U 26067.00844755 +.00000000 +00000-0 +11420-3 0 00007
2 27640 98.7162 75.4270 0014700 141.0826 219.1412 14.19912142 07
| Epoch (UTC): | 08 March 2026 00:12:09 |
| Eccentricity: | 0.0014700 |
| inclination: | 98.7162° |
| perigee height: | 815 km |
| apogee height: | 836 km |
| right ascension of ascending node: | 75.4270° |
| argument of perigee: | 141.0826° |
| revolutions per day: | 14.19912142 |
| mean anomaly at epoch: | 219.1412° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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