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AE5RC

In orbit NORAD 66677 EVWL-1878-8170-5974-4826

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
AE5RC
Status
Active
The satellite is in orbit
The network has not received data from this satellite for a long time
Launch and timeline
Carrier rocket
Falcon 9 Block 5
Spaceport
Space Launch Complex 4E
Launch time
Separation time
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
483.93 km
Apogee
488.91 km
Inclination
97.4°
Period
94.4 min
Semi-major axis
6864.5 km
Velocity
7.62 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-14 06:09:04 UTC
Two-line elements (TLE)
1 66677U 25276M   26286.78321478  .00015265  00000-0  60562-3 0  9999
2 66677 97.4071 359.3832 0003643 330.4477 29.6555 15.25451869 48515
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Orbit history, past year

Mean elements of every TLE set over the past 365 days, plotted against the epoch of the set. Each source is its own line; click it in the legend to hide it. A jump in altitude is a manoeuvre or a bad set; lines drifting apart are a disagreement between sources. “TLE age” is how many hours have passed since the epoch of the source's freshest set, plotted against when the set reached us, on a logarithmic scale. A set the source repeats unchanged does not reset the age.

Prediction divergence

Each TLE set is propagated with SGP4 to the epoch of the next set from the same source and compared with it, plotted against the epoch of the next set; the tooltip shows how many hours ahead the prediction ran. The logarithmic scale shows the size of the divergence and the tooltip its sign: plus along-track means the prediction is ahead of the satellite. This is how well the sets agree, not the true error: the reference is a TLE too, off by about a kilometre. An outlier is a manoeuvre between sets. Sets more than a week apart are not compared.

Time of closest approach, UTC Object 1 Object 2 Distance, km Speed, km/s Max. probability
2026-10-14 08:59:54 OTP-2
NORAD 63235
AE5RC
NORAD 66677
1.865 15.11 4.5e-07
2026-10-14 10:34:22 OTP-2
NORAD 63235
AE5RC
NORAD 66677
2.142 15.11 3.4e-07
2026-10-14 12:08:49 OTP-2
NORAD 63235
AE5RC
NORAD 66677
2.429 15.11 2.7e-07
2026-10-14 13:43:17 OTP-2
NORAD 63235
AE5RC
NORAD 66677
2.726 15.11 2.1e-07
2026-10-14 15:17:44 OTP-2
NORAD 63235
AE5RC
NORAD 66677
3.030 15.11 1.7e-07
2026-10-14 16:52:12 OTP-2
NORAD 63235
AE5RC
NORAD 66677
3.341 15.11 1.4e-07
2026-10-14 18:26:40 OTP-2
NORAD 63235
AE5RC
NORAD 66677
3.659 15.11 1.2e-07
2026-10-14 20:01:07 OTP-2
NORAD 63235
AE5RC
NORAD 66677
3.983 15.11 9.9e-08
2026-10-14 21:35:35 OTP-2
NORAD 63235
AE5RC
NORAD 66677
4.313 15.11 8.4e-08
2026-10-14 23:10:02 OTP-2
NORAD 63235
AE5RC
NORAD 66677
4.648 15.11 7.3e-08
2026-10-15 00:44:30 OTP-2
NORAD 63235
AE5RC
NORAD 66677
4.989 15.11 6.3e-08
2026-10-15 01:52:56 AE5RC
NORAD 66677
YINLI-1 R/B
NORAD 100138
3.227 1.68 4.2e-07
2026-10-15 16:10:52 AE5RC
NORAD 66677
WESTFORD NEEDLES
NORAD 2367
4.674 3.98 1.9e-07
2026-10-16 06:11:57 OBJECT G
NORAD 63297
AE5RC
NORAD 66677
3.644 9.04 2.8e-07
2026-10-18 20:27:15 AE5RC
NORAD 66677
HADES-SA (SPINNYONE)
NORAD 68446
4.138 12.79 1.6e-07
2026-10-18 21:57:05 AE5RC
NORAD 66677
AE5RB
NORAD 66693
2.732 0.01 5.9e-07
2026-10-18 22:50:33 AE5RC
NORAD 66677
AE5RB
NORAD 66693
3.645 0.01 5.9e-06
2026-10-18 23:32:58 AE5RC
NORAD 66677
AE5RB
NORAD 66693
0.865 0.01 5.9e-06
2026-10-19 00:19:40 AE5RC
NORAD 66677
AE5RB
NORAD 66693
0.995 0.01 5.9e-06
2026-10-19 00:24:54 AE5RC
NORAD 66677
ASAP-S
NORAD 38013
3.535 13.84 1.8e-07
2026-10-19 01:09:51 AE5RC
NORAD 66677
AE5RB
NORAD 66693
4.413 0.01 2.3e-07
2026-10-19 01:50:29 AE5RC
NORAD 66677
AE5RB
NORAD 66693
3.348 0.01 3.9e-07
2026-10-19 16:05:41 ZHUHAI-1 OHS-02
NORAD 43441
AE5RC
NORAD 66677
4.427 7.03 2.0e-07
2026-10-19 20:00:32 PHASMA-LAMARR
NORAD 66673
AE5RC
NORAD 66677
0.919 0.01 5.2e-06
2026-10-19 21:46:17 STARLINK-5617
NORAD 55753
AE5RC
NORAD 66677
3.693 5.40 9.2e-06

Data: CelesTrak SOCRATES Plus, computed from TLEs of the public catalog. This is an estimate, not grounds for a manoeuvre: TLEs carry no covariance, and the maximum probability assumes a position error.

All conjunctions of this satellite