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 49155U 26145.47077094 +.00000000 +00000-0 +33669-5 0 00005
2 49155 70.0006 60.8557 0003243 269.0351 91.0437 14.98331299 01
| Epoch (UTC): | 25 May 2026 11:17:54 |
| Eccentricity: | 0.0003243 |
| inclination: | 70.0006° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 60.8557° |
| argument of perigee: | 269.0351° |
| revolutions per day: | 14.98331299 |
| mean anomaly at epoch: | 91.0437° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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