▸Orbital parameters

Orbit class	SSO
Inclination	97.3767°
Eccentricity	0.0004222
Period	91.7 min
Apogee	362 km
Perigee	357 km
Mean motion	15.69808668 rev/day
RAAN	281.4527°
Arg of perigee	187.0911°
Mean anomaly	173.0292°
B*	7.7662e-4
Rev at epoch	10,590

▸Two-line element set (TLE)

EPOCH Jul 6, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 60520U 24149BE 26187.25930828 .00093238 00000-0 77662-3 0 9990

2 60520 97.3767 281.4527 0004222 187.0911 173.0292 15.69808668105906

▸ source OMM (JSON)

{
  "OBJECT_NAME": "IPERDRONE.0",
  "OBJECT_ID": "2024-149BE",
  "EPOCH": "2026-07-06T06:13:24.235+00:00",
  "MEAN_MOTION": 15.69808668,
  "ECCENTRICITY": 0.00042223,
  "INCLINATION": 97.3767,
  "RA_OF_ASC_NODE": 281.4527,
  "ARG_OF_PERICENTER": 187.0911,
  "MEAN_ANOMALY": 173.0292,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 60520,
  "REV_AT_EPOCH": 10590,
  "BSTAR": 0.00077662499,
  "MEAN_MOTION_DOT": 0.00093238,
  "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	IPERDRONE.0
Operator	Italian Space AgencyHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Italy
Launch date	Aug 16, 2024HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	12HIGHvia 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/60520

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