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 53484U 26145.23500719 +.00000000 +00000-0 +88274-5 0 00006
2 53484 97.4467 266.2607 0001817 112.9380 247.2039 15.05654263 07
| Epoch (UTC): | 25 May 2026 05:38:24 |
| Eccentricity: | 0.0001817 |
| inclination: | 97.4467° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 266.2607° |
| argument of perigee: | 112.9380° |
| revolutions per day: | 15.05654263 |
| mean anomaly at epoch: | 247.2039° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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