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 28366U 26133.42524242 +.00000000 +00000-0 +39184-4 0 00007
2 28366 98.0988 301.3789 0105445 355.7563 4.2721 14.38023486 08
| Epoch (UTC): | 13 May 2026 10:12:20 |
| Eccentricity: | 0.0105445 |
| inclination: | 98.0988° |
| perigee height: | 690 km |
| apogee height: | 840 km |
| right ascension of ascending node: | 301.3789° |
| argument of perigee: | 355.7563° |
| revolutions per day: | 14.38023486 |
| mean anomaly at epoch: | 4.2721° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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