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 28096U 26158.74981220 +.00000000 +00000-0 +80174-4 0 00007
2 28096 63.6811 58.9672 0070308 107.3254 253.5479 13.41070638 07
| Epoch (UTC): | 07 June 2026 17:59:43 |
| Eccentricity: | 0.0070308 |
| inclination: | 63.6811° |
| perigee height: | 1053 km |
| apogee height: | 1158 km |
| right ascension of ascending node: | 58.9672° |
| argument of perigee: | 107.3254° |
| revolutions per day: | 13.41070638 |
| mean anomaly at epoch: | 253.5479° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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