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 62325U 26145.62838517 +.00000000 +00000-0 +17923-4 0 00005
2 62325 86.4983 350.7579 0001479 85.1000 275.0303 13.24407650 01
| Epoch (UTC): | 25 May 2026 15:04:52 |
| Eccentricity: | 0.0001479 |
| inclination: | 86.4983° |
| perigee height: | 1167 km |
| apogee height: | 1169 km |
| right ascension of ascending node: | 350.7579° |
| argument of perigee: | 85.1000° |
| revolutions per day: | 13.24407650 |
| mean anomaly at epoch: | 275.0303° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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