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 13028U 26074.54585061 +.00000000 +00000-0 +11076-3 0 00008
2 13028 74.0382 262.2950 0020182 274.9195 84.9656 14.39879849 06
| Epoch (UTC): | 15 March 2026 13:06:01 |
| Eccentricity: | 0.0020182 |
| inclination: | 74.0382° |
| perigee height: | 744 km |
| apogee height: | 773 km |
| right ascension of ascending node: | 262.2950° |
| argument of perigee: | 274.9195° |
| revolutions per day: | 14.39879849 |
| mean anomaly at epoch: | 84.9656° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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