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 53403U 26145.41571676 +.00000000 +00000-0 -98150-4 0 00001
2 53403 53.2126 140.0312 0001134 89.9933 270.1189 15.08842804 05
| Epoch (UTC): | 25 May 2026 09:58:37 |
| Eccentricity: | 0.0001134 |
| inclination: | 53.2126° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 140.0312° |
| argument of perigee: | 89.9933° |
| revolutions per day: | 15.08842804 |
| mean anomaly at epoch: | 270.1189° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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