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 44048U 26145.25621236 +.00000000 +00000-0 +00000-0 0 00008
2 44048 0.0121 116.1305 0004061 347.7940 17.1666 1.00268199 01
| Epoch (UTC): | 25 May 2026 06:08:56 |
| Eccentricity: | 0.0004061 |
| inclination: | 0.0121° |
| perigee height: | 35770 km |
| apogee height: | 35805 km |
| right ascension of ascending node: | 116.1305° |
| argument of perigee: | 347.7940° |
| revolutions per day: | 1.00268199 |
| mean anomaly at epoch: | 17.1666° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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