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 00029U 26109.27910973 +.00000000 +00000-0 +66230-4 0 00001
2 00029 48.3786 304.5903 0022013 13.9734 346.1784 14.78700411 04
| Epoch (UTC): | 19 April 2026 06:41:55 |
| Eccentricity: | 0.0022013 |
| inclination: | 48.3786° |
| perigee height: | 618 km |
| apogee height: | 649 km |
| right ascension of ascending node: | 304.5903° |
| argument of perigee: | 13.9734° |
| revolutions per day: | 14.78700411 |
| mean anomaly at epoch: | 346.1784° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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