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 49384U 26145.61870110 +.00000000 +00000-0 +12779-3 0 00002
2 49384 98.2435 279.4135 0000970 76.9464 283.1846 14.64169444 09
| Epoch (UTC): | 25 May 2026 14:50:55 |
| Eccentricity: | 0.0000970 |
| inclination: | 98.2435° |
| perigee height: | 679 km |
| apogee height: | 680 km |
| right ascension of ascending node: | 279.4135° |
| argument of perigee: | 76.9464° |
| revolutions per day: | 14.64169444 |
| mean anomaly at epoch: | 283.1846° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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