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 28738U 26039.56501275 +.00000000 +00000-0 +49767-3 0 00008
2 28738 97.3624 53.7019 0007424 117.0510 243.1504 15.57594009 02
| Epoch (UTC): | 08 February 2026 13:33:37 |
| Eccentricity: | 0.0007424 |
| inclination: | 97.3624° |
| perigee height: | 390 km |
| apogee height: | 400 km |
| right ascension of ascending node: | 53.7019° |
| argument of perigee: | 117.0510° |
| revolutions per day: | 15.57594009 |
| mean anomaly at epoch: | 243.1504° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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