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 55362U 26145.24488684 +.00000000 +00000-0 +13476-4 0 00001
2 55362 43.0017 216.1747 0001432 279.5911 80.4779 15.27576541 08
| Epoch (UTC): | 25 May 2026 05:52:38 |
| Eccentricity: | 0.0001432 |
| inclination: | 43.0017° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 216.1747° |
| argument of perigee: | 279.5911° |
| revolutions per day: | 15.27576541 |
| mean anomaly at epoch: | 80.4779° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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