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 22827U 26032.12004449 +.00000000 +00000-0 +90305-4 0 00002
2 22827 98.6583 100.8844 0009827 71.1916 307.4968 14.32485960 07
| Epoch (UTC): | 01 February 2026 02:52:51 |
| Eccentricity: | 0.0009827 |
| inclination: | 98.6583° |
| perigee height: | 776 km |
| apogee height: | 790 km |
| right ascension of ascending node: | 100.8844° |
| argument of perigee: | 71.1916° |
| revolutions per day: | 14.32485960 |
| mean anomaly at epoch: | 307.4968° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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