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 49027U 26145.57689985 +.00000000 +00000-0 +29150-3 0 00000
2 49027 34.9996 355.0859 0006189 219.9978 140.0278 15.10288560 06
| Epoch (UTC): | 25 May 2026 13:50:44 |
| Eccentricity: | 0.0006189 |
| inclination: | 34.9996° |
| perigee height: | 531 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 355.0859° |
| argument of perigee: | 219.9978° |
| revolutions per day: | 15.10288560 |
| mean anomaly at epoch: | 140.0278° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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