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 08820U 26097.14477860 +.00000000 +00000-0 +00000-0 0 00002
2 08820 109.8104 155.0248 0044671 317.4965 55.8389 6.38664837 04
| Epoch (UTC): | 07 April 2026 03:28:28 |
| Eccentricity: | 0.0044671 |
| inclination: | 109.8104° |
| perigee height: | 5838 km |
| apogee height: | 5948 km |
| right ascension of ascending node: | 155.0248° |
| argument of perigee: | 317.4965° |
| revolutions per day: | 6.38664837 |
| mean anomaly at epoch: | 55.8389° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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