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 08800U 26020.06558410 +.00000000 +00000-0 +36159-4 0 00006
2 08800 81.2489 42.8604 0093261 296.7600 62.4051 14.10641822 02
| Epoch (UTC): | 20 January 2026 01:34:26 |
| Eccentricity: | 0.0093261 |
| inclination: | 81.2489° |
| perigee height: | 790 km |
| apogee height: | 925 km |
| right ascension of ascending node: | 42.8604° |
| argument of perigee: | 296.7600° |
| revolutions per day: | 14.10641822 |
| mean anomaly at epoch: | 62.4051° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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