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 44204U 26132.76772565 +.00000000 +00000-0 +00000-0 0 00006
2 44204 58.6468 38.0171 0023857 234.3090 349.8662 1.00250503 03
| Epoch (UTC): | 12 May 2026 18:25:31 |
| Eccentricity: | 0.0023857 |
| inclination: | 58.6468° |
| perigee height: | 35692 km |
| apogee height: | 35893 km |
| right ascension of ascending node: | 38.0171° |
| argument of perigee: | 234.3090° |
| revolutions per day: | 1.00250503 |
| mean anomaly at epoch: | 349.8662° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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