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 28870U 26044.63738220 +.00000000 +00000-0 +10839-2 0 00008
2 28870 49.3465 194.6611 5376001 104.6703 318.3698 4.98659686 08
| Epoch (UTC): | 13 February 2026 15:17:49 |
| Eccentricity: | 0.5376001 |
| inclination: | 49.3465° |
| perigee height: | 314 km |
| apogee height: | 15874 km |
| right ascension of ascending node: | 194.6611° |
| argument of perigee: | 104.6703° |
| revolutions per day: | 4.98659686 |
| mean anomaly at epoch: | 318.3698° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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