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 27843U 26150.47128904 +.00000000 +00000-0 +65377-4 0 00008
2 27843 98.7044 158.4444 0008900 308.0314 52.0059 14.21318478 04
| Epoch (UTC): | 30 May 2026 11:18:39 |
| Eccentricity: | 0.0008900 |
| inclination: | 98.7044° |
| perigee height: | 814 km |
| apogee height: | 827 km |
| right ascension of ascending node: | 158.4444° |
| argument of perigee: | 308.0314° |
| revolutions per day: | 14.21318478 |
| mean anomaly at epoch: | 52.0059° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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