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 53421U 26145.25370647 +.00000000 +00000-0 -24861-3 0 00005
2 53421 53.2144 130.4076 0001228 84.9111 275.2022 15.08860147 04
| Epoch (UTC): | 25 May 2026 06:05:20 |
| Eccentricity: | 0.0001228 |
| inclination: | 53.2144° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 130.4076° |
| argument of perigee: | 84.9111° |
| revolutions per day: | 15.08860147 |
| mean anomaly at epoch: | 275.2022° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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