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 49318U 26145.61560889 +.00000000 +00000-0 +75084-4 0 00007
2 49318 97.4529 182.5383 0013793 43.7279 316.4981 14.00148624 00
| Epoch (UTC): | 25 May 2026 14:46:28 |
| Eccentricity: | 0.0013793 |
| inclination: | 97.4529° |
| perigee height: | 883 km |
| apogee height: | 903 km |
| right ascension of ascending node: | 182.5383° |
| argument of perigee: | 43.7279° |
| revolutions per day: | 14.00148624 |
| mean anomaly at epoch: | 316.4981° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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