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 26159.13777902 +.00000000 +00000-0 +77401-4 0 00008
2 13649 74.0002 86.4137 0018580 197.0264 267.7609 14.38659483 06
| Epoch (UTC): | 08 June 2026 03:18:24 |
| Eccentricity: | 0.0018580 |
| inclination: | 74.0002° |
| perigee height: | 750 km |
| apogee height: | 776 km |
| right ascension of ascending node: | 86.4137° |
| argument of perigee: | 197.0264° |
| revolutions per day: | 14.38659483 |
| mean anomaly at epoch: | 267.7609° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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