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 53807U 26135.29934213 +.00000000 +00000-0 +98616-4 0 00000
2 53807 53.2283 188.3183 0007436 75.8539 284.3292 15.37852027 07
| Epoch (UTC): | 15 May 2026 07:11:03 |
| Eccentricity: | 0.0007436 |
| inclination: | 53.2283° |
| perigee height: | 447 km |
| apogee height: | 458 km |
| right ascension of ascending node: | 188.3183° |
| argument of perigee: | 75.8539° |
| revolutions per day: | 15.37852027 |
| mean anomaly at epoch: | 284.3292° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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