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 62527U 26145.48819772 +.00000000 +00000-0 +55716-3 0 00006
2 62527 42.9993 146.1811 0001469 279.9474 80.1211 15.27590977 09
| Epoch (UTC): | 25 May 2026 11:43:00 |
| Eccentricity: | 0.0001469 |
| inclination: | 42.9993° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 146.1811° |
| argument of perigee: | 279.9474° |
| revolutions per day: | 15.27590977 |
| mean anomaly at epoch: | 80.1211° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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