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 13649U 26100.04415308 +.00000000 +00000-0 +78195-4 0 00004
2 13649 74.0010 195.6021 0019048 314.3879 219.4137 14.38641537 07
| Epoch (UTC): | 10 April 2026 01:03:34 |
| Eccentricity: | 0.0019048 |
| inclination: | 74.0010° |
| perigee height: | 749 km |
| apogee height: | 777 km |
| right ascension of ascending node: | 195.6021° |
| argument of perigee: | 314.3879° |
| revolutions per day: | 14.38641537 |
| mean anomaly at epoch: | 219.4137° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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