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 26073.22576332 +.00000000 +00000-0 +13057-3 0 00004
2 13028 74.0383 264.7335 0020178 277.4913 82.3950 14.39879067 03
| Epoch (UTC): | 14 March 2026 05:25:05 |
| Eccentricity: | 0.0020178 |
| inclination: | 74.0383° |
| perigee height: | 744 km |
| apogee height: | 773 km |
| right ascension of ascending node: | 264.7335° |
| argument of perigee: | 277.4913° |
| revolutions per day: | 14.39879067 |
| mean anomaly at epoch: | 82.3950° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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