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 53998U 26145.51311764 +.00000000 +00000-0 +18890-4 0 00003
2 53998 53.2132 229.0070 0001066 89.5798 270.5317 15.08837023 03
| Epoch (UTC): | 25 May 2026 12:18:53 |
| Eccentricity: | 0.0001066 |
| inclination: | 53.2132° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 229.0070° |
| argument of perigee: | 89.5798° |
| revolutions per day: | 15.08837023 |
| mean anomaly at epoch: | 270.5317° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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