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 26067.94540480 +.00000000 +00000-0 +11765-3 0 00005
2 13028 74.0384 274.4869 0020164 287.9535 71.9422 14.39874522 04
| Epoch (UTC): | 08 March 2026 22:41:22 |
| Eccentricity: | 0.0020164 |
| inclination: | 74.0384° |
| perigee height: | 745 km |
| apogee height: | 773 km |
| right ascension of ascending node: | 274.4869° |
| argument of perigee: | 287.9535° |
| revolutions per day: | 14.39874522 |
| mean anomaly at epoch: | 71.9422° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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