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 53492U 26145.66668980 +.00000000 +00000-0 +44218-2 0 00004
2 53492 97.6010 266.6478 0001285 94.2135 280.6415 15.26440801 04
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001285 |
| inclination: | 97.6010° |
| perigee height: | 486 km |
| apogee height: | 487 km |
| right ascension of ascending node: | 266.6478° |
| argument of perigee: | 94.2135° |
| revolutions per day: | 15.26440801 |
| mean anomaly at epoch: | 280.6415° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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