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 53225U 26145.59362120 +.00000000 +00000-0 +96663-3 0 00009
2 53225 97.4483 206.5989 0001888 113.5511 246.5914 15.05587959 00
| Epoch (UTC): | 25 May 2026 14:14:48 |
| Eccentricity: | 0.0001888 |
| inclination: | 97.4483° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 206.5989° |
| argument of perigee: | 113.5511° |
| revolutions per day: | 15.05587959 |
| mean anomaly at epoch: | 246.5914° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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