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 52353U 26145.59732538 +.00000000 +00000-0 +25897-3 0 00005
2 52353 53.2117 213.8687 0001284 81.4687 278.6451 15.08845992 07
| Epoch (UTC): | 25 May 2026 14:20:08 |
| Eccentricity: | 0.0001284 |
| inclination: | 53.2117° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 213.8687° |
| argument of perigee: | 81.4687° |
| revolutions per day: | 15.08845992 |
| mean anomaly at epoch: | 278.6451° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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