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 53733U 26145.08629955 +.00000000 +00000-0 -17661-4 0 00002
2 53733 53.2136 271.3928 0001042 78.6985 281.4124 15.08847993 01
| Epoch (UTC): | 25 May 2026 02:04:16 |
| Eccentricity: | 0.0001042 |
| inclination: | 53.2136° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 271.3928° |
| argument of perigee: | 78.6985° |
| revolutions per day: | 15.08847993 |
| mean anomaly at epoch: | 281.4124° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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