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 04420U 26128.20942483 +.00000000 +00000-0 +14623-3 0 00003
2 04420 81.2327 36.0648 0087488 24.2605 336.2647 14.12619839 01
| Epoch (UTC): | 08 May 2026 05:01:34 |
| Eccentricity: | 0.0087488 |
| inclination: | 81.2327° |
| perigee height: | 787 km |
| apogee height: | 914 km |
| right ascension of ascending node: | 36.0648° |
| argument of perigee: | 24.2605° |
| revolutions per day: | 14.12619839 |
| mean anomaly at epoch: | 336.2647° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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