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 08027U 26088.08672037 +.00000000 +00000-0 +70304-4 0 00005
2 08027 81.2984 206.0529 0057071 237.6417 121.9222 14.07766590 09
| Epoch (UTC): | 29 March 2026 02:04:52 |
| Eccentricity: | 0.0057071 |
| inclination: | 81.2984° |
| perigee height: | 826 km |
| apogee height: | 908 km |
| right ascension of ascending node: | 206.0529° |
| argument of perigee: | 237.6417° |
| revolutions per day: | 14.07766590 |
| mean anomaly at epoch: | 121.9222° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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