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 26157.12105983 +.00000000 +00000-0 +81384-4 0 00004
2 13649 73.9999 90.1400 0018664 201.1990 262.8513 14.38658566 01
| Epoch (UTC): | 06 June 2026 02:54:19 |
| Eccentricity: | 0.0018664 |
| inclination: | 73.9999° |
| perigee height: | 750 km |
| apogee height: | 776 km |
| right ascension of ascending node: | 90.1400° |
| argument of perigee: | 201.1990° |
| revolutions per day: | 14.38658566 |
| mean anomaly at epoch: | 262.8513° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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