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 26145.18419876 +.00000000 +00000-0 +51011-4 0 00002
2 28366 98.0996 312.4691 0104708 320.0849 39.2673 14.38026540 03
| Epoch (UTC): | 25 May 2026 04:25:14 |
| Eccentricity: | 0.0104708 |
| inclination: | 98.0996° |
| perigee height: | 690 km |
| apogee height: | 840 km |
| right ascension of ascending node: | 312.4691° |
| argument of perigee: | 320.0849° |
| revolutions per day: | 14.38026540 |
| mean anomaly at epoch: | 39.2673° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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