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 44819U 26145.64037994 +.00000000 +00000-0 +51045-4 0 00008
2 44819 97.8105 152.6155 0002497 97.8755 262.2741 14.80436684 04
| Epoch (UTC): | 25 May 2026 15:22:08 |
| Eccentricity: | 0.0002497 |
| inclination: | 97.8105° |
| perigee height: | 626 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 152.6155° |
| argument of perigee: | 97.8755° |
| revolutions per day: | 14.80436684 |
| mean anomaly at epoch: | 262.2741° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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