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 27561U 26128.18506350 +.00000000 +00000-0 +67281-4 0 00009
2 27561 98.4627 348.1182 0042955 253.0419 106.6069 14.58541258 06
| Epoch (UTC): | 08 May 2026 04:26:29 |
| Eccentricity: | 0.0042955 |
| inclination: | 98.4627° |
| perigee height: | 667 km |
| apogee height: | 728 km |
| right ascension of ascending node: | 348.1182° |
| argument of perigee: | 253.0419° |
| revolutions per day: | 14.58541258 |
| mean anomaly at epoch: | 106.6069° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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