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 28352U 26067.10332525 +.00000000 +00000-0 -85259-4 0 00009
2 28352 71.0010 310.7842 0012153 285.8857 74.0924 14.12145503 03
| Epoch (UTC): | 08 March 2026 02:28:47 |
| Eccentricity: | 0.0012153 |
| inclination: | 71.0010° |
| perigee height: | 843 km |
| apogee height: | 861 km |
| right ascension of ascending node: | 310.7842° |
| argument of perigee: | 285.8857° |
| revolutions per day: | 14.12145503 |
| mean anomaly at epoch: | 74.0924° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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