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 54051U 26145.01826406 +.00000000 +00000-0 +64652-4 0 00000
2 54051 53.2186 1.7065 0001382 95.4577 264.6573 15.09038370 01
| Epoch (UTC): | 25 May 2026 00:26:18 |
| Eccentricity: | 0.0001382 |
| inclination: | 53.2186° |
| perigee height: | 538 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 1.7065° |
| argument of perigee: | 95.4577° |
| revolutions per day: | 15.09038370 |
| mean anomaly at epoch: | 264.6573° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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