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 28353U 26068.52772257 +.00000000 +00000-0 -10049-3 0 00001
2 28353 70.9995 232.8323 0004032 9.7045 350.4154 14.14598066 05
| Epoch (UTC): | 09 March 2026 12:39:55 |
| Eccentricity: | 0.0004032 |
| inclination: | 70.9995° |
| perigee height: | 841 km |
| apogee height: | 847 km |
| right ascension of ascending node: | 232.8323° |
| argument of perigee: | 9.7045° |
| revolutions per day: | 14.14598066 |
| mean anomaly at epoch: | 350.4154° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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