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 00053U 26106.50552343 +.00000000 +00000-0 +19378-3 0 00004
2 00053 47.2767 172.6054 0100963 252.9750 105.9955 12.17409197 02
| Epoch (UTC): | 16 April 2026 12:07:57 |
| Eccentricity: | 0.0100963 |
| inclination: | 47.2767° |
| perigee height: | 1523 km |
| apogee height: | 1684 km |
| right ascension of ascending node: | 172.6054° |
| argument of perigee: | 252.9750° |
| revolutions per day: | 12.17409197 |
| mean anomaly at epoch: | 105.9955° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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