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 53491U 26145.66668980 +.00000000 +00000-0 +97957-2 0 00001
2 53491 97.6053 268.0648 0001212 85.5583 302.4924 15.47802281 00
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001212 |
| inclination: | 97.6053° |
| perigee height: | 422 km |
| apogee height: | 424 km |
| right ascension of ascending node: | 268.0648° |
| argument of perigee: | 85.5583° |
| revolutions per day: | 15.47802281 |
| mean anomaly at epoch: | 302.4924° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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