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 26021.39431884 +.00000000 +00000-0 +15611-3 0 00005
2 13028 74.0415 0.4554 0018601 22.7090 337.4883 14.39838532 03
| Epoch (UTC): | 21 January 2026 09:27:49 |
| Eccentricity: | 0.0018601 |
| inclination: | 74.0415° |
| perigee height: | 746 km |
| apogee height: | 772 km |
| right ascension of ascending node: | 0.4554° |
| argument of perigee: | 22.7090° |
| revolutions per day: | 14.39838532 |
| mean anomaly at epoch: | 337.4883° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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