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 52897U 26088.19693345 +.00000000 +00000-0 +23969-3 0 00000
2 52897 98.2084 232.4040 0007330 276.8191 83.2177 14.63160052 02
| Epoch (UTC): | 29 March 2026 04:43:35 |
| Eccentricity: | 0.0007330 |
| inclination: | 98.2084° |
| perigee height: | 678 km |
| apogee height: | 688 km |
| right ascension of ascending node: | 232.4040° |
| argument of perigee: | 276.8191° |
| revolutions per day: | 14.63160052 |
| mean anomaly at epoch: | 83.2177° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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