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 14820U 26088.08619522 +.00000000 +00000-0 +65231-4 0 00006
2 14820 82.5418 226.8195 0016475 269.1858 90.7471 14.85996662 04
| Epoch (UTC): | 29 March 2026 02:04:07 |
| Eccentricity: | 0.0016475 |
| inclination: | 82.5418° |
| perigee height: | 599 km |
| apogee height: | 622 km |
| right ascension of ascending node: | 226.8195° |
| argument of perigee: | 269.1858° |
| revolutions per day: | 14.85996662 |
| mean anomaly at epoch: | 90.7471° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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