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 62651U 26145.46821112 +.00000000 +00000-0 +40175-3 0 00006
2 62651 97.3993 228.0255 0002539 68.1025 292.0485 15.30132952 08
| Epoch (UTC): | 25 May 2026 11:14:13 |
| Eccentricity: | 0.0002539 |
| inclination: | 97.3993° |
| perigee height: | 474 km |
| apogee height: | 477 km |
| right ascension of ascending node: | 228.0255° |
| argument of perigee: | 68.1025° |
| revolutions per day: | 15.30132952 |
| mean anomaly at epoch: | 292.0485° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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