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 49158U 26145.19317472 +.00000000 +00000-0 +51282-3 0 00003
2 49158 69.9641 318.3957 0002995 197.4938 162.6157 15.73705303 08
| Epoch (UTC): | 25 May 2026 04:38:10 |
| Eccentricity: | 0.0002995 |
| inclination: | 69.9641° |
| perigee height: | 346 km |
| apogee height: | 350 km |
| right ascension of ascending node: | 318.3957° |
| argument of perigee: | 197.4938° |
| revolutions per day: | 15.73705303 |
| mean anomaly at epoch: | 162.6157° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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