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 62388U 26145.19816713 +.00000000 +00000-0 +23637-3 0 00008
2 62388 45.0015 75.9221 0000597 283.5182 76.5632 15.21095480 04
| Epoch (UTC): | 25 May 2026 04:45:21 |
| Eccentricity: | 0.0000597 |
| inclination: | 45.0015° |
| perigee height: | 502 km |
| apogee height: | 503 km |
| right ascension of ascending node: | 75.9221° |
| argument of perigee: | 283.5182° |
| revolutions per day: | 15.21095480 |
| mean anomaly at epoch: | 76.5632° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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