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 26076.02858252 +.00000000 +00000-0 -77981-4 0 00003
2 28352 70.9985 292.1286 0012059 274.5831 85.3913 14.12142658 00
| Epoch (UTC): | 17 March 2026 00:41:09 |
| Eccentricity: | 0.0012059 |
| inclination: | 70.9985° |
| perigee height: | 843 km |
| apogee height: | 861 km |
| right ascension of ascending node: | 292.1286° |
| argument of perigee: | 274.5831° |
| revolutions per day: | 14.12142658 |
| mean anomaly at epoch: | 85.3913° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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