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 22220U 26049.85428763 +.00000000 +00000-0 -27460-4 0 00009
2 22220 70.9976 228.0490 0011133 130.9495 330.2774 14.16854689 01
| Epoch (UTC): | 18 February 2026 20:30:10 |
| Eccentricity: | 0.0011133 |
| inclination: | 70.9976° |
| perigee height: | 828 km |
| apogee height: | 844 km |
| right ascension of ascending node: | 228.0490° |
| argument of perigee: | 130.9495° |
| revolutions per day: | 14.16854689 |
| mean anomaly at epoch: | 330.2774° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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