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 13068U 26064.11249514 +.00000000 +00000-0 +27015-3 0 00004
2 13068 81.1767 166.1339 0022365 192.7668 167.3001 15.21959090 05
| Epoch (UTC): | 05 March 2026 02:41:59 |
| Eccentricity: | 0.0022365 |
| inclination: | 81.1767° |
| perigee height: | 485 km |
| apogee height: | 515 km |
| right ascension of ascending node: | 166.1339° |
| argument of perigee: | 192.7668° |
| revolutions per day: | 15.21959090 |
| mean anomaly at epoch: | 167.3001° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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