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 60463U 26145.63811375 +.00000000 +00000-0 +45201-3 0 00009
2 60463 34.9926 292.0801 0007987 8.3819 351.7030 15.31880696 02
| Epoch (UTC): | 25 May 2026 15:18:53 |
| Eccentricity: | 0.0007987 |
| inclination: | 34.9926° |
| perigee height: | 465 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 292.0801° |
| argument of perigee: | 8.3819° |
| revolutions per day: | 15.31880696 |
| mean anomaly at epoch: | 351.7030° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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