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 53414U 26145.33466266 +.00000000 +00000-0 +88948-5 0 00006
2 53414 53.2117 130.0429 0000494 131.5749 228.5286 15.08839675 09
| Epoch (UTC): | 25 May 2026 08:01:54 |
| Eccentricity: | 0.0000494 |
| inclination: | 53.2117° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 130.0429° |
| argument of perigee: | 131.5749° |
| revolutions per day: | 15.08839675 |
| mean anomaly at epoch: | 228.5286° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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