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 02180U 26087.93986329 +.00000000 +00000-0 +29491-4 0 00005
2 02180 90.2185 80.5555 0077018 213.6974 145.9297 14.01079347 04
| Epoch (UTC): | 28 March 2026 22:33:24 |
| Eccentricity: | 0.0077018 |
| inclination: | 90.2185° |
| perigee height: | 834 km |
| apogee height: | 946 km |
| right ascension of ascending node: | 80.5555° |
| argument of perigee: | 213.6974° |
| revolutions per day: | 14.01079347 |
| mean anomaly at epoch: | 145.9297° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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