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 49008U 26145.58179264 +.00000000 +00000-0 -25227-4 0 00007
2 49008 98.7499 149.2425 0002324 124.0288 236.1109 14.19901247 02
| Epoch (UTC): | 25 May 2026 13:57:46 |
| Eccentricity: | 0.0002324 |
| inclination: | 98.7499° |
| perigee height: | 824 km |
| apogee height: | 827 km |
| right ascension of ascending node: | 149.2425° |
| argument of perigee: | 124.0288° |
| revolutions per day: | 14.19901247 |
| mean anomaly at epoch: | 236.1109° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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