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 49018U 26145.64805730 +.00000000 +00000-0 +12025-3 0 00009
2 49018 45.0012 328.9237 0007574 123.5196 236.6365 14.08532634 07
| Epoch (UTC): | 25 May 2026 15:33:12 |
| Eccentricity: | 0.0007574 |
| inclination: | 45.0012° |
| perigee height: | 859 km |
| apogee height: | 870 km |
| right ascension of ascending node: | 328.9237° |
| argument of perigee: | 123.5196° |
| revolutions per day: | 14.08532634 |
| mean anomaly at epoch: | 236.6365° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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