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 53214U 26145.63102166 +.00000000 +00000-0 +12099-3 0 00005
2 53214 97.4474 205.5386 0001242 123.3941 236.7405 15.05648601 06
| Epoch (UTC): | 25 May 2026 15:08:40 |
| Eccentricity: | 0.0001242 |
| inclination: | 97.4474° |
| perigee height: | 549 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 205.5386° |
| argument of perigee: | 123.3941° |
| revolutions per day: | 15.05648601 |
| mean anomaly at epoch: | 236.7405° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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