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 26072.01157777 +.00000000 +00000-0 +99454-4 0 00009
2 27640 98.7161 80.3544 0014891 127.4545 232.7988 14.19914173 07
| Epoch (UTC): | 13 March 2026 00:16:40 |
| Eccentricity: | 0.0014891 |
| inclination: | 98.7161° |
| perigee height: | 815 km |
| apogee height: | 836 km |
| right ascension of ascending node: | 80.3544° |
| argument of perigee: | 127.4545° |
| revolutions per day: | 14.19914173 |
| mean anomaly at epoch: | 232.7988° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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