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 62867U 26145.38362970 +.00000000 +00000-0 +38214-3 0 00009
2 62867 53.1573 133.2693 0001203 88.2076 271.9063 15.30204733 05
| Epoch (UTC): | 25 May 2026 09:12:25 |
| Eccentricity: | 0.0001203 |
| inclination: | 53.1573° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 133.2693° |
| argument of perigee: | 88.2076° |
| revolutions per day: | 15.30204733 |
| mean anomaly at epoch: | 271.9063° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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