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 26018.56526536 +.00000000 +00000-0 +98756-3 0 00001
2 28870 49.3494 213.7342 5382306 88.3176 329.6094 4.98325137 07
| Epoch (UTC): | 18 January 2026 13:33:58 |
| Eccentricity: | 0.5382306 |
| inclination: | 49.3494° |
| perigee height: | 308 km |
| apogee height: | 15893 km |
| right ascension of ascending node: | 213.7342° |
| argument of perigee: | 88.3176° |
| revolutions per day: | 4.98325137 |
| mean anomaly at epoch: | 329.6094° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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