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 26049.81144132 +.00000000 +00000-0 +84553-4 0 00001
2 13028 74.0415 307.9785 0019740 324.1338 35.8491 14.39862364 07
| Epoch (UTC): | 18 February 2026 19:28:28 |
| Eccentricity: | 0.0019740 |
| inclination: | 74.0415° |
| perigee height: | 745 km |
| apogee height: | 773 km |
| right ascension of ascending node: | 307.9785° |
| argument of perigee: | 324.1338° |
| revolutions per day: | 14.39862364 |
| mean anomaly at epoch: | 35.8491° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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