▸Orbital parameters

Orbit class	SSO
Inclination	97.3745°
Eccentricity	0.0002099
Period	94.5 min
Apogee	496 km
Perigee	493 km
Mean motion	15.23700125 rev/day
RAAN	264.0177°
Arg of perigee	159.6473°
Mean anomaly	200.4848°
B*	1.3548e-4
Rev at epoch	10,482

▸Two-line element set (TLE)

EPOCH Jul 7, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 60472U 24149E 26188.06120890 .00003182 00000-0 13548-3 0 9998

2 60472 97.3745 264.0177 0002099 159.6473 200.4848 15.23700125104825

▸ source OMM (JSON)

{
  "OBJECT_NAME": "CONNECTA IOT-1",
  "OBJECT_ID": "2024-149E",
  "EPOCH": "2026-07-07T01:28:08.449+00:00",
  "MEAN_MOTION": 15.23700125,
  "ECCENTRICITY": 0.0002099,
  "INCLINATION": 97.3745,
  "RA_OF_ASC_NODE": 264.0177,
  "ARG_OF_PERICENTER": 159.6473,
  "MEAN_ANOMALY": 200.4848,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 60472,
  "REV_AT_EPOCH": 10482,
  "BSTAR": 0.00013548,
  "MEAN_MOTION_DOT": 0.00003182,
  "MEAN_MOTION_DDOT": 0
}

Reconstructed from CelesTrak OMM mean-elements (element-set number is a placeholder). TLE/OMM data is approximate. Not for operational use or collision avoidance.

▸Satellite metadata

Name	CONNECTA IOT-1
Operator	Plan-S Satellite and Space TechnologiesHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Türkiye
Launch date	Aug 16, 2024HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	10HIGHvia GCAT — Jonathan McDowell's General Catalog
Mission purpose	—
Object class	PAYLOADHIGH

▸Data quality

Score85 / 100

Claims7

Sources1

TLEavailable

▸Sources

GCAT — Jonathan McDowell's General CatalogCC BY 4.0planet4589.org

▸Actions

GET /api/v1/satellites/60472

//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.