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 28493U 26103.33667522 +.00000000 +00000-0 +11040-3 0 00004
2 28493 98.2168 238.4546 0004961 131.0141 229.1499 14.80027790 09
| Epoch (UTC): | 13 April 2026 08:04:48 |
| Eccentricity: | 0.0004961 |
| inclination: | 98.2168° |
| perigee height: | 626 km |
| apogee height: | 633 km |
| right ascension of ascending node: | 238.4546° |
| argument of perigee: | 131.0141° |
| revolutions per day: | 14.80027790 |
| mean anomaly at epoch: | 229.1499° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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