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 27600U 26087.86950098 +.00000000 +00000-0 +85799-4 0 00008
2 27600 98.8048 53.4881 0010511 178.2958 181.8262 14.30820167 01
| Epoch (UTC): | 28 March 2026 20:52:04 |
| Eccentricity: | 0.0010511 |
| inclination: | 98.8048° |
| perigee height: | 781 km |
| apogee height: | 797 km |
| right ascension of ascending node: | 53.4881° |
| argument of perigee: | 178.2958° |
| revolutions per day: | 14.30820167 |
| mean anomaly at epoch: | 181.8262° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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