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 00053U 26141.14611714 +.00000000 +00000-0 -26808-3 0 00008
2 00053 47.2783 65.7450 0100948 355.6121 4.3776 12.17412495 06
| Epoch (UTC): | 21 May 2026 03:30:24 |
| Eccentricity: | 0.0100948 |
| inclination: | 47.2783° |
| perigee height: | 1523 km |
| apogee height: | 1684 km |
| right ascension of ascending node: | 65.7450° |
| argument of perigee: | 355.6121° |
| revolutions per day: | 12.17412495 |
| mean anomaly at epoch: | 4.3776° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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