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 28894U 26038.91619993 +.00000000 +00000-0 +17096-3 0 00006
2 28894 98.2848 177.7148 0015216 328.4673 31.5617 14.65201676 06
| Epoch (UTC): | 07 February 2026 21:59:19 |
| Eccentricity: | 0.0015216 |
| inclination: | 98.2848° |
| perigee height: | 666 km |
| apogee height: | 687 km |
| right ascension of ascending node: | 177.7148° |
| argument of perigee: | 328.4673° |
| revolutions per day: | 14.65201676 |
| mean anomaly at epoch: | 31.5617° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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