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 49056U 26145.59317514 +.00000000 +00000-0 +00000-0 0 00000
2 49056 0.0177 15.2274 0002344 45.7561 83.4372 1.00272956 02
| Epoch (UTC): | 25 May 2026 14:14:10 |
| Eccentricity: | 0.0002344 |
| inclination: | 0.0177° |
| perigee height: | 35776 km |
| apogee height: | 35796 km |
| right ascension of ascending node: | 15.2274° |
| argument of perigee: | 45.7561° |
| revolutions per day: | 1.00272956 |
| mean anomaly at epoch: | 83.4372° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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