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 52994U 26145.20769625 +.00000000 +00000-0 -66687-4 0 00005
2 52994 53.2132 110.6203 0001645 108.4447 251.6725 15.08851840 02
| Epoch (UTC): | 25 May 2026 04:59:04 |
| Eccentricity: | 0.0001645 |
| inclination: | 53.2132° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 110.6203° |
| argument of perigee: | 108.4447° |
| revolutions per day: | 15.08851840 |
| mean anomaly at epoch: | 251.6725° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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