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 49163U 26145.52948363 +.00000000 +00000-0 +85224-4 0 00009
2 49163 70.0002 81.7477 0003066 270.5668 89.5139 14.97533210 07
| Epoch (UTC): | 25 May 2026 12:42:27 |
| Eccentricity: | 0.0003066 |
| inclination: | 70.0002° |
| perigee height: | 572 km |
| apogee height: | 577 km |
| right ascension of ascending node: | 81.7477° |
| argument of perigee: | 270.5668° |
| revolutions per day: | 14.97533210 |
| mean anomaly at epoch: | 89.5139° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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