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 26099.76632049 +.00000000 +00000-0 +93701-4 0 00004
2 13028 74.0412 215.7127 0019893 224.9869 134.9676 14.39898035 05
| Epoch (UTC): | 09 April 2026 18:23:30 |
| Eccentricity: | 0.0019893 |
| inclination: | 74.0412° |
| perigee height: | 745 km |
| apogee height: | 773 km |
| right ascension of ascending node: | 215.7127° |
| argument of perigee: | 224.9869° |
| revolutions per day: | 14.39898035 |
| mean anomaly at epoch: | 134.9676° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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