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 28059U 26038.95066139 +.00000000 +00000-0 +15227-3 0 00005
2 28059 98.6848 32.6968 0047504 323.6614 36.1359 14.54986943 08
| Epoch (UTC): | 07 February 2026 22:48:57 |
| Eccentricity: | 0.0047504 |
| inclination: | 98.6848° |
| perigee height: | 676 km |
| apogee height: | 743 km |
| right ascension of ascending node: | 32.6968° |
| argument of perigee: | 323.6614° |
| revolutions per day: | 14.54986943 |
| mean anomaly at epoch: | 36.1359° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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