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 28895U 26071.36632001 +.00000000 +00000-0 +38474-3 0 00001
2 28895 98.2836 225.0408 0014868 149.4116 210.7960 14.72334173 04
| Epoch (UTC): | 12 March 2026 08:47:30 |
| Eccentricity: | 0.0014868 |
| inclination: | 98.2836° |
| perigee height: | 643 km |
| apogee height: | 664 km |
| right ascension of ascending node: | 225.0408° |
| argument of perigee: | 149.4116° |
| revolutions per day: | 14.72334173 |
| mean anomaly at epoch: | 210.7960° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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