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 49071U 26145.36945455 +.00000000 +00000-0 +80378-4 0 00003
2 49071 97.4809 148.8977 0001797 112.7357 247.4066 15.16736538 08
| Epoch (UTC): | 25 May 2026 08:52:00 |
| Eccentricity: | 0.0001797 |
| inclination: | 97.4809° |
| perigee height: | 514 km |
| apogee height: | 517 km |
| right ascension of ascending node: | 148.8977° |
| argument of perigee: | 112.7357° |
| revolutions per day: | 15.16736538 |
| mean anomaly at epoch: | 247.4066° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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