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 52200U 26145.61245358 +.00000000 +00000-0 +67732-5 0 00004
2 52200 98.4071 154.5207 0000954 86.9628 273.1671 14.42219902 02
| Epoch (UTC): | 25 May 2026 14:41:55 |
| Eccentricity: | 0.0000954 |
| inclination: | 98.4071° |
| perigee height: | 750 km |
| apogee height: | 752 km |
| right ascension of ascending node: | 154.5207° |
| argument of perigee: | 86.9628° |
| revolutions per day: | 14.42219902 |
| mean anomaly at epoch: | 273.1671° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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