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 28352U 26041.95687705 +.00000000 +00000-0 -10206-3 0 00006
2 28352 71.0046 3.3361 0011992 317.4137 42.6053 14.12155194 07
| Epoch (UTC): | 10 February 2026 22:57:54 |
| Eccentricity: | 0.0011992 |
| inclination: | 71.0046° |
| perigee height: | 843 km |
| apogee height: | 861 km |
| right ascension of ascending node: | 3.3361° |
| argument of perigee: | 317.4137° |
| revolutions per day: | 14.12155194 |
| mean anomaly at epoch: | 42.6053° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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