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 53486U 26145.66668980 +.00000000 +00000-0 +16800-1 0 00002
2 53486 97.6051 267.8574 0001472 108.8187 87.3002 15.41697062 03
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001472 |
| inclination: | 97.6051° |
| perigee height: | 440 km |
| apogee height: | 442 km |
| right ascension of ascending node: | 267.8574° |
| argument of perigee: | 108.8187° |
| revolutions per day: | 15.41697062 |
| mean anomaly at epoch: | 87.3002° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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