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 26021.77520752 +.00000000 +00000-0 +14591-2 0 00006
2 28870 49.3467 211.3835 5381658 90.3348 328.4099 4.98371731 04
| Epoch (UTC): | 21 January 2026 18:36:17 |
| Eccentricity: | 0.5381658 |
| inclination: | 49.3467° |
| perigee height: | 308 km |
| apogee height: | 15891 km |
| right ascension of ascending node: | 211.3835° |
| argument of perigee: | 90.3348° |
| revolutions per day: | 4.98371731 |
| mean anomaly at epoch: | 328.4099° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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