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 27597U 26079.86442206 +.00000000 +00000-0 +11876-3 0 00005
2 27597 98.7789 38.4206 0001125 28.4412 331.6831 14.29293116 06
| Epoch (UTC): | 20 March 2026 20:44:46 |
| Eccentricity: | 0.0001125 |
| inclination: | 98.7789° |
| perigee height: | 793 km |
| apogee height: | 795 km |
| right ascension of ascending node: | 38.4206° |
| argument of perigee: | 28.4412° |
| revolutions per day: | 14.29293116 |
| mean anomaly at epoch: | 331.6831° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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