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 49028U 26145.17753434 +.00000000 +00000-0 +17371-3 0 00000
2 49028 34.9942 53.0359 0001254 268.3168 91.7397 15.02541028 01
| Epoch (UTC): | 25 May 2026 04:15:38 |
| Eccentricity: | 0.0001254 |
| inclination: | 34.9942° |
| perigee height: | 558 km |
| apogee height: | 560 km |
| right ascension of ascending node: | 53.0359° |
| argument of perigee: | 268.3168° |
| revolutions per day: | 15.02541028 |
| mean anomaly at epoch: | 91.7397° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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