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 28898U 26159.36344126 +.00000000 +00000-0 +11640-3 0 00005
2 28898 98.3528 303.6631 0018584 12.1928 347.9720 14.64383189 02
| Epoch (UTC): | 08 June 2026 08:43:21 |
| Eccentricity: | 0.0018584 |
| inclination: | 98.3528° |
| perigee height: | 666 km |
| apogee height: | 692 km |
| right ascension of ascending node: | 303.6631° |
| argument of perigee: | 12.1928° |
| revolutions per day: | 14.64383189 |
| mean anomaly at epoch: | 347.9720° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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